Parameterization of Stillinger-Weber Potential for Two-Dimensional Atomic Crystals
Jin-Wu Jiang, Yu-Ping Zhou

TL;DR
This paper develops parameter sets for the Stillinger-Weber potential tailored to 156 two-dimensional atomic crystals, enabling efficient nonlinear simulations of their physical and mechanical properties.
Contribution
It introduces a systematic method to derive Stillinger-Weber potential parameters from the valence force field model for a wide range of 2D materials.
Findings
Parameters for 156 2D crystals are provided.
Resources include code and files for various simulations.
Potential enables accurate nonlinear physical modeling.
Abstract
We parametrize the Stillinger-Weber potential for 156 two-dimensional atomic crystals. Parameters for the Stillinger-Weber potential are obtained from the valence force field model following the analytic approach (Nanotechnology 26, 315706 (2015)), in which the valence force constants are determined by the phonon spectrum. The Stillinger-Weber potential is an efficient nonlinear interaction, and is applicable for numerical simulations of nonlinear physical or mechanical processes. The supplemental resources for all simulations in the present work are available online in Ref. 1, including a fortran code to generate crystals' structures, files for molecular dynamics simulations using LAMMPS, files for phonon calculations with the Stillinger-Weber potential using GULP, and files for phonon calculations with the valence force field model using GULP.
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.417 | 4.825 | 4.825 | 4.825 |
| or | 2.090 | 98.222 | 58.398 | 98.222 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-O | 7.506 | 1.380 | 9.540 | 0.0 | 2.939 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 63.576 | 98.222 | 1.380 | 1.380 | 0.0 | 2.939 | 0.0 | 2.939 | 0.0 | 3.460 | |
| 85.850 | 58.398 | 1.380 | 1.380 | 0.0 | 2.939 | 0.0 | 2.939 | 0.0 | 3.460 | |
| 63.576 | 98.222 | 1.380 | 1.380 | 0.0 | 2.939 | 0.0 | 2.939 | 0.0 | 3.460 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc1-O1-O1 | 1.000 | 1.380 | 2.129 | 0.000 | 1.000 | 0.000 | 7.506 | 2.627 | 4 | 0 | 0.0 |
| Sc1-O1-O3 | 1.000 | 0.000 | 0.000 | 63.576 | 1.000 | -0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Sc1-O1-O2 | 1.000 | 0.000 | 0.000 | 85.850 | 1.000 | 0.524 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Sc1-Sc3 | 1.000 | 0.000 | 0.000 | 63.576 | 1.000 | -0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 5.192 | 2.027 | 2.027 | 2.027 |
| or | 2.520 | 94.467 | 64.076 | 94.467 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-S | 5.505 | 1.519 | 20.164 | 0.0 | 3.498 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 22.768 | 94.467 | 1.519 | 1.519 | 0.0 | 3.498 | 0.0 | 3.498 | 0.0 | 4.132 | |
| 27.977 | 64.076 | 1.519 | 1.519 | 0.0 | 3.498 | 0.0 | 3.498 | 0.0 | 4.132 | |
| 22.768 | 94.467 | 1.519 | 1.519 | 0.0 | 3.498 | 0.0 | 3.498 | 0.0 | 4.132 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc1-S1-S1 | 1.000 | 1.519 | 2.303 | 0.000 | 1.000 | 0.000 | 5.505 | 3.784 | 4 | 0 | 0.0 |
| Sc1-S1-S3 | 1.000 | 0.000 | 0.000 | 22.768 | 1.000 | -0.078 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Sc1-S1-S2 | 1.000 | 0.000 | 0.000 | 27.977 | 1.000 | 0.437 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Sc1-Sc3 | 1.000 | 0.000 | 0.000 | 22.768 | 1.000 | -0.078 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 5.192 | 2.027 | 2.027 | 2.027 |
| or | 2.650 | 92.859 | 66.432 | 92.859 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-Se | 5.853 | 1.533 | 24.658 | 0.0 | 3.658 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 21.292 | 92.859 | 1.533 | 1.533 | 0.0 | 3.658 | 0.0 | 3.658 | 0.0 | 4.327 | |
| 25.280 | 66.432 | 1.533 | 1.533 | 0.0 | 3.658 | 0.0 | 3.658 | 0.0 | 4.327 | |
| 21.292 | 92.859 | 1.533 | 1.533 | 0.0 | 3.658 | 0.0 | 3.658 | 0.0 | 4.327 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc1-Se1-Se1 | 1.000 | 1.533 | 2.386 | 0.000 | 1.000 | 0.000 | 5.853 | 4.464 | 4 | 0 | 0.0 |
| Sc1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 21.292 | 1.000 | -0.050 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Sc1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 25.280 | 1.000 | 0.400 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Sc1-Sc3 | 1.000 | 0.000 | 0.000 | 21.292 | 1.000 | -0.050 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 5.192 | 2.027 | 2.027 | 2.027 |
| or | 2.890 | 77.555 | 87.364 | 87.364 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-Te | 4.630 | 1.050 | 34.879 | 0.0 | 3.761 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 11.848 | 77.555 | 1.050 | 1.050 | 0.0 | 3.761 | 0.0 | 3.761 | 0.0 | 4.504 | |
| 11.322 | 87.364 | 1.050 | 1.050 | 0.0 | 3.761 | 0.0 | 3.761 | 0.0 | 4.504 | |
| 11.848 | 77.555 | 1.050 | 1.050 | 0.0 | 3.761 | 0.0 | 3.761 | 0.0 | 4.504 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc1-Te1-Te1 | 1.000 | 1.050 | 3.581 | 0.000 | 1.000 | 0.000 | 4.630 | 28.679 | 4 | 0 | 0.0 |
| Sc1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 11.848 | 1.000 | 0.216 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Sc1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 11.322 | 1.000 | 0.046 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Sc1-Sc3 | 1.000 | 0.000 | 0.000 | 11.848 | 1.000 | 0.216 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 4.782 | 3.216 | 3.216 | 3.216 |
| or | 2.750 | 82.323 | 81.071 | 82.323 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ti-Te | 4.414 | 1.173 | 28.596 | 0.0 | 3.648 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 22.321 | 82.323 | 1.173 | 1.173 | 0.0 | 3.648 | 0.0 | 3.648 | 0.0 | 4.354 | |
| 22.463 | 81.071 | 1.173 | 1.173 | 0.0 | 3.648 | 0.0 | 3.648 | 0.0 | 4.354 | |
| 11.321 | 82.323 | 1.173 | 1.173 | 0.0 | 3.648 | 0.0 | 3.648 | 0.0 | 4.354 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ti1-Te1-Te1 | 1.000 | 1.173 | 3.110 | 0.000 | 1.000 | 0.000 | 4.414 | 15.100 | 4 | 0 | 0.0 |
| Ti1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 22.321 | 1.000 | 0.134 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ti1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 22.463 | 1.000 | 0.155 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Ti1-Ti3 | 1.000 | 0.000 | 0.000 | 22.321 | 1.000 | 0.134 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.417 | 4.825 | 4.825 | 4.825 |
| or | 1.920 | 89.356 | 71.436 | 89.356 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-O | 5.105 | 1.011 | 6.795 | 0.0 | 2.617 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 43.951 | 89.356 | 1.011 | 1.011 | 0.0 | 2.617 | 0.0 | 2.617 | 0.0 | 3.105 | |
| 48.902 | 71.436 | 1.011 | 1.011 | 0.0 | 2.617 | 0.0 | 2.617 | 0.0 | 3.105 | |
| 43.951 | 89.356 | 1.011 | 1.011 | 0.0 | 2.617 | 0.0 | 2.617 | 0.0 | 3.105 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V1-O1-O1 | 1.000 | 1.011 | 2.589 | 0.000 | 1.000 | 0.000 | 5.105 | 6.509 | 4 | 0 | 0.0 |
| V1-O1-O3 | 1.000 | 0.000 | 0.000 | 43.951 | 1.000 | 0.011 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| V1-O1-O2 | 1.000 | 0.000 | 0.000 | 48.902 | 1.000 | 0.318 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-V1-V3 | 1.000 | 0.000 | 0.000 | 43.951 | 1.000 | 0.011 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.392 | 4.074 | 4.074 | 4.074 |
| or | 2.310 | 83.954 | 78.878 | 83.954 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-S | 5.714 | 1.037 | 14.237 | 0.0 | 3.084 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.059 | 83.954 | 1.037 | 1.037 | 0.0 | 3.084 | 0.0 | 3.084 | 0.0 | 3.676 | |
| 30.874 | 78.878 | 1.037 | 1.037 | 0.0 | 3.084 | 0.0 | 3.084 | 0.0 | 3.676 | |
| 30.059 | 83.954 | 1.037 | 1.037 | 0.0 | 3.084 | 0.0 | 3.084 | 0.0 | 3.676 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V1-S1-S1 | 1.000 | 1.037 | 2.973 | 0.000 | 1.000 | 0.000 | 5.714 | 12.294 | 4 | 0 | 0.0 |
| V1-S1-S3 | 1.000 | 0.000 | 0.000 | 30.059 | 1.000 | 0.105 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| V1-S1-S2 | 1.000 | 0.000 | 0.000 | 30.874 | 1.000 | 0.193 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-V1-V3 | 1.000 | 0.000 | 0.000 | 30.059 | 1.000 | 0.105 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.492 | 4.716 | 4.716 | 4.716 |
| or | 2.450 | 82.787 | 80.450 | 82.787 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-Se | 4.817 | 1.061 | 18.015 | 0.0 | 3.256 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 33.299 | 82.787 | 1.061 | 1.061 | 0.0 | 3.256 | 0.0 | 3.256 | 0.0 | 3.884 | |
| 33.702 | 80.450 | 1.061 | 1.061 | 0.0 | 3.256 | 0.0 | 3.256 | 0.0 | 3.884 | |
| 33.299 | 82.787 | 1.061 | 1.061 | 0.0 | 3.256 | 0.0 | 3.256 | 0.0 | 3.884 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V1-Se1-Se1 | 1.000 | 1.061 | 3.070 | 0.000 | 1.000 | 0.000 | 4.817 | 14.236 | 4 | 0 | 0.0 |
| V1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 33.299 | 1.000 | 0.126 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| V1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 33.702 | 1.000 | 0.166 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-V1-V3 | 1.000 | 0.000 | 0.000 | 33.299 | 1.000 | 0.126 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.371 | 4.384 | 4.384 | 4.384 |
| or | 2.660 | 81.708 | 81.891 | 81.708 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-Te | 5.410 | 1.112 | 25.032 | 0.0 | 3.520 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 29.743 | 81.708 | 1.112 | 1.112 | 0.0 | 3.520 | 0.0 | 3.520 | 0.0 | 4.203 | |
| 29.716 | 81.891 | 1.112 | 1.112 | 0.0 | 3.520 | 0.0 | 3.520 | 0.0 | 4.203 | |
| 29.743 | 81.708 | 1.112 | 1.112 | 0.0 | 3.520 | 0.0 | 3.520 | 0.0 | 4.203 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V1-Te1-Te1 | 1.000 | 1.112 | 3.164 | 0.000 | 1.000 | 0.000 | 5.410 | 16.345 | 4 | 0 | 0.0 |
| V1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 29.743 | 1.000 | 0.144 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| V1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 29.716 | 1.000 | 0.141 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-V1-V3 | 1.000 | 0.000 | 0.000 | 29.743 | 1.000 | 0.144 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 12.881 | 8.039 | 8.039 | 8.039 |
| or | 1.880 | 86.655 | 75.194 | 86.655 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Cr-O | 6.343 | 0.916 | 6.246 | 0.0 | 2.536 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 65.805 | 86.655 | 0.916 | 0.916 | 0.0 | 2.536 | 0.0 | 2.536 | 0.0 | 3.016 | |
| 70.163 | 75.194 | 0.916 | 0.916 | 0.0 | 2.536 | 0.0 | 2.536 | 0.0 | 3.016 | |
| 65.805 | 86.655 | 0.916 | 0.916 | 0.0 | 2.536 | 0.0 | 2.536 | 0.0 | 3.016 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Cr1-O1-O1 | 1.000 | 0.916 | 2.769 | 0.000 | 1.000 | 0.000 | 6.242 | 8.871 | 4 | 0 | 0.0 |
| Cr1-O1-O3 | 1.000 | 0.000 | 0.000 | 65.805 | 1.000 | 0.058 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Cr1-O1-O2 | 1.000 | 0.000 | 0.000 | 70.163 | 1.000 | 0.256 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Cr1-Cr3 | 1.000 | 0.000 | 0.000 | 65.805 | 1.000 | 0.058 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.752 | 4.614 | 4.614 | 4.614 |
| or | 2.254 | 83.099 | 80.031 | 83.099 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Cr-S | 5.544 | 0.985 | 12.906 | 0.0 | 2.999 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.963 | 83.099 | 0.985 | 0.985 | 0.0 | 2.999 | 0.0 | 2.999 | 0.0 | 3.577 | |
| 33.491 | 80.031 | 0.985 | 0.985 | 0.0 | 2.999 | 0.0 | 2.999 | 0.0 | 3.577 | |
| 32.963 | 83.099 | 0.985 | 0.985 | 0.0 | 2.999 | 0.0 | 2.999 | 0.0 | 3.577 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Cr1-S1-S1 | 1.000 | 0.985 | 3.043 | 0.000 | 1.000 | 0.000 | 5.544 | 13.683 | 4 | 0 | 0.0 |
| Cr1-S1-S3 | 1.000 | 0.000 | 0.000 | 32.963 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Cr1-S1-S2 | 1.000 | 0.000 | 0.000 | 33.491 | 1.000 | 0.173 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Cr1-Cr3 | 1.000 | 0.000 | 0.000 | 32.963 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.542 | 4.465 | 4.465 | 4.465 |
| or | 2.380 | 82.229 | 81.197 | 82.229 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Cr-Se | 6.581 | 1.012 | 16.043 | 0.0 | 3.156 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.881 | 82.229 | 1.012 | 1.012 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.767 | |
| 31.044 | 81.197 | 1.012 | 1.012 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.767 | |
| 30.881 | 82.229 | 1.012 | 1.012 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.767 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Cr1-Se1-Se1 | 1.000 | 1.012 | 3.118 | 0.000 | 1.000 | 0.000 | 6.581 | 15.284 | 4 | 0 | 0.0 |
| Cr1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 30.881 | 1.000 | 0.135 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Cr1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 31.044 | 1.000 | 0.153 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Cr1-Cr3 | 1.000 | 0.000 | 0.000 | 30.881 | 1.000 | 0.135 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.197 | 4.543 | 4.543 | 4.543 |
| or | 2.580 | 82.139 | 81.316 | 82.139 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Cr-Te | 6.627 | 1.094 | 22.154 | 0.0 | 3.420 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 31.316 | 82.139 | 1.094 | 1.094 | 0.0 | 3.420 | 0.0 | 3.420 | 0.0 | 4.082 | |
| 31.447 | 81.316 | 1.094 | 1.094 | 0.0 | 3.420 | 0.0 | 3.420 | 0.0 | 4.082 | |
| 31.316 | 82.139 | 1.094 | 1.094 | 0.0 | 3.420 | 0.0 | 3.420 | 0.0 | 4.082 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Cr1-Te1-Te1 | 1.000 | 1.094 | 3.126 | 0.000 | 1.000 | 0.000 | 6.627 | 15.461 | 4 | 0 | 0.0 |
| Cr1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 31.316 | 1.000 | 0.137 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Cr1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 31.447 | 1.000 | 0.151 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Cr1-Cr3 | 1.000 | 0.000 | 0.000 | 31.316 | 1.000 | 0.137 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.382 | 6.253 | 6.253 | 6.253 |
| or | 1.870 | 88.511 | 72.621 | 88.511 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mn-O | 4.721 | 0.961 | 6.114 | 0.0 | 2.540 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 55.070 | 88.511 | 0.961 | 0.961 | 0.0 | 2.540 | 0.0 | 2.540 | 0.0 | 3.016 | |
| 60.424 | 72.621 | 0.961 | 0.961 | 0.0 | 2.540 | 0.0 | 2.540 | 0.0 | 3.016 | |
| 55.070 | 88.511 | 0.961 | 0.961 | 0.0 | 2.540 | 0.0 | 2.540 | 0.0 | 3.016 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mn1-O1-O1 | 1.000 | 0.961 | 2.643 | 0.000 | 1.000 | 0.000 | 4.721 | 7.158 | 4 | 0 | 0.0 |
| Mn1-O1-O3 | 1.000 | 0.000 | 0.000 | 55.070 | 1.000 | 0.026 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Mn1-O1-O2 | 1.000 | 0.000 | 0.000 | 60.424 | 1.000 | 0.299 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Mn1-Mn3 | 1.000 | 0.000 | 0.000 | 55.070 | 1.000 | 0.026 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.377 | 3.213 | 3.213 | 3.213 |
| or | 1.880 | 88.343 | 72.856 | 88.343 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Fe-O | 4.242 | 0.962 | 6.246 | 0.0 | 2.552 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 28.105 | 88.343 | 0.962 | 0.962 | 0.0 | 2.552 | 0.0 | 2.552 | 0.0 | 3.031 | |
| 30.754 | 72.856 | 0.962 | 0.962 | 0.0 | 2.552 | 0.0 | 2.552 | 0.0 | 3.031 | |
| 28.105 | 88.343 | 0.962 | 0.962 | 0.0 | 2.552 | 0.0 | 2.552 | 0.0 | 3.031 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Fe1-O1-O1 | 1.000 | 0.962 | 2.654 | 0.000 | 1.000 | 0.000 | 4.242 | 7.298 | 4 | 0 | 0.0 |
| Fe1-O1-O3 | 1.000 | 0.000 | 0.000 | 28.105 | 1.000 | 0.029 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Fe1-O1-O2 | 1.000 | 0.000 | 0.000 | 30.754 | 1.000 | 0.295 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Fe1-Fe3 | 1.000 | 0.000 | 0.000 | 28.105 | 1.000 | 0.029 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.338 | 3.964 | 3.964 | 3.964 |
| or | 2.220 | 87.132 | 74.537 | 87.132 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Fe-S | 4.337 | 1.097 | 12.145 | 0.0 | 3.000 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 33.060 | 87.132 | 1.097 | 1.097 | 0.0 | 3.000 | 0.0 | 3.000 | 0.0 | 3.567 | |
| 35.501 | 74.537 | 1.097 | 1.097 | 0.0 | 3.000 | 0.0 | 3.000 | 0.0 | 3.567 | |
| 33.060 | 87.132 | 1.097 | 1.097 | 0.0 | 3.000 | 0.0 | 3.000 | 0.0 | 3.567 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Fe1-S1-S1 | 1.000 | 1.097 | 2.735 | 0.000 | 1.000 | 0.000 | 4.337 | 8.338 | 4 | 0 | 0.0 |
| Fe1-S1-S3 | 1.000 | 0.000 | 0.000 | 33.060 | 1.000 | 0.050 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Fe1-S1-S2 | 1.000 | 0.000 | 0.000 | 35.501 | 1.000 | 0.267 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Fe1-Fe3 | 1.000 | 0.000 | 0.000 | 33.060 | 1.000 | 0.050 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.338 | 3.964 | 3.964 | 3.964 |
| or | 2.350 | 86.488 | 75.424 | 86.488 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Fe-Se | 4.778 | 1.139 | 15.249 | 0.0 | 3.168 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.235 | 86.488 | 1.139 | 1.139 | 0.0 | 3.168 | 0.0 | 3.168 | 0.0 | 3.768 | |
| 34.286 | 75.424 | 1.139 | 1.139 | 0.0 | 3.168 | 0.0 | 3.168 | 0.0 | 3.768 | |
| 32.235 | 86.488 | 1.139 | 1.139 | 0.0 | 3.168 | 0.0 | 3.168 | 0.0 | 3.768 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Fe1-Se1-Se1 | 1.000 | 1.139 | 2.781 | 0.000 | 1.000 | 0.000 | 4.778 | 9.049 | 4 | 0 | 0.0 |
| Fe1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 32.235 | 1.000 | 0.061 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Fe1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 34.286 | 1.000 | 0.252 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Fe1-Fe3 | 1.000 | 0.000 | 0.000 | 32.235 | 1.000 | 0.061 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.338 | 3.964 | 3.964 | 3.964 |
| or | 2.530 | 86.904 | 74.851 | 86.904 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Fe-Te | 5.599 | 1.242 | 20.486 | 0.0 | 3.416 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.766 | 86.904 | 1.242 | 1.242 | 0.0 | 3.416 | 0.0 | 3.416 | 0.0 | 4.062 | |
| 35.065 | 74.851 | 1.242 | 1.242 | 0.0 | 3.416 | 0.0 | 3.416 | 0.0 | 4.062 | |
| 32.766 | 86.904 | 1.242 | 1.242 | 0.0 | 3.416 | 0.0 | 3.416 | 0.0 | 4.062 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Fe1-Te1-Te1 | 1.000 | 1.242 | 2.751 | 0.000 | 1.000 | 0.000 | 5.599 | 8.615 | 4 | 0 | 0.0 |
| Fe1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 32.766 | 1.000 | 0.054 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Fe1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 35.065 | 1.000 | 0.261 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Fe1-Fe3 | 1.000 | 0.000 | 0.000 | 32.766 | 1.000 | 0.054 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.712 | 2.656 | 2.656 | 2.656 |
| or | 2.510 | 89.046 | 71.873 | 89.046 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Co-Te | 6.169 | 1.310 | 19.846 | 0.0 | 3.417 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 23.895 | 89.046 | 1.310 | 1.310 | 0.0 | 3.417 | 0.0 | 3.417 | 0.0 | 4.055 | |
| 26.449 | 71.873 | 1.310 | 1.310 | 0.0 | 3.417 | 0.0 | 3.417 | 0.0 | 4.055 | |
| 23.895 | 89.046 | 1.310 | 1.310 | 0.0 | 3.417 | 0.0 | 3.417 | 0.0 | 4.055 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Co1-Te1-Te1 | 1.000 | 1.310 | 2.608 | 0.000 | 1.000 | 0.000 | 6.169 | 6.739 | 4 | 0 | 0.0 |
| Co1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 23.895 | 1.000 | 0.017 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Co1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 26.449 | 1.000 | 0.311 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Co1-Co3 | 1.000 | 0.000 | 0.000 | 23.895 | 1.000 | 0.017 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.933 | 3.418 | 3.418 | 3.418 |
| or | 2.240 | 98.740 | 57.593 | 98.740 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-S | 6.425 | 1.498 | 12.588 | 0.0 | 3.156 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 46.062 | 98.740 | 1.498 | 1.498 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.713 | |
| 63.130 | 57.593 | 1.498 | 1.498 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.713 | |
| 46.062 | 98.740 | 1.498 | 1.498 | 0.0 | 3.156 | 0.0 | 3.156 | 0.0 | 3.713 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni1-S1-S1 | 1.000 | 1.498 | 2.107 | 0.000 | 1.000 | 0.000 | 6.425 | 2.502 | 4 | 0 | 0.0 |
| Ni1-S1-S3 | 1.000 | 0.000 | 0.000 | 46.062 | 1.000 | -0.152 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ni1-S1-S2 | 1.000 | 0.000 | 0.000 | 63.130 | 1.000 | 0.536 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Ni1-Ni3 | 1.000 | 0.000 | 0.000 | 46.062 | 1.000 | -0.152 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 4.823 | 2.171 | 2.171 | 2.171 |
| or | 2.350 | 90.228 | 70.206 | 90.228 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-Se | 4.004 | 1.267 | 15.249 | 0.0 | 3.213 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 20.479 | 90.228 | 1.267 | 1.267 | 0.0 | 3.213 | 0.0 | 3.213 | 0.0 | 3.809 | |
| 23.132 | 70.206 | 1.267 | 1.267 | 0.0 | 3.213 | 0.0 | 3.213 | 0.0 | 3.809 | |
| 20.479 | 90.228 | 1.267 | 1.267 | 0.0 | 3.213 | 0.0 | 3.213 | 0.0 | 3.809 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni1-Se1-Se1 | 1.000 | 1.267 | 2.535 | 0.000 | 1.000 | 0.000 | 4.004 | 5.913 | 4 | 0 | 0.0 |
| Ni1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 20.479 | 1.000 | -0.004 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ni1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 23.132 | 1.000 | 0.339 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Ni1-Ni3 | 1.000 | 0.000 | 0.000 | 20.479 | 1.000 | -0.004 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.712 | 2.656 | 2.656 | 2.656 |
| or | 2.540 | 89.933 | 70.624 | 89.933 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-Te | 6.461 | 1.359 | 20.812 | 0.0 | 3.469 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 24.759 | 89.933 | 1.359 | 1.359 | 0.0 | 3.469 | 0.0 | 3.469 | 0.0 | 4.114 | |
| 27.821 | 70.624 | 1.359 | 1.359 | 0.0 | 3.469 | 0.0 | 3.469 | 0.0 | 4.114 | |
| 24.759 | 89.933 | 1.359 | 1.359 | 0.0 | 3.469 | 0.0 | 3.469 | 0.0 | 4.114 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni1-Te1-Te1 | 1.000 | 1.359 | 2.553 | 0.000 | 1.000 | 0.000 | 6.461 | 6.107 | 4 | 0 | 0.0 |
| Ni1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 24.759 | 1.000 | 0.001 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ni1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 27.821 | 1.000 | 0.332 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Ni1-Ni3 | 1.000 | 0.000 | 0.000 | 24.759 | 1.000 | 0.001 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.230 | 4.811 | 4.811 | 4.811 |
| or | 2.470 | 84.140 | 78.626 | 84.140 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Nb-S | 6.439 | 1.116 | 18.610 | 0.0 | 3.300 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 35.748 | 84.140 | 1.116 | 1.116 | 0.0 | 3.300 | 0.0 | 3.300 | 0.0 | 3.933 | |
| 36.807 | 78.626 | 1.116 | 1.116 | 0.0 | 3.300 | 0.0 | 3.300 | 0.0 | 3.933 | |
| 35.748 | 84.140 | 1.116 | 1.116 | 0.0 | 3.300 | 0.0 | 3.300 | 0.0 | 3.933 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nb1-S1-S1 | 1.000 | 1.116 | 2.958 | 0.000 | 1.000 | 0.000 | 6.439 | 12.014 | 4 | 0 | 0.0 |
| Nb1-S1-S3 | 1.000 | 0.000 | 0.000 | 35.748 | 1.000 | 0.102 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Nb1-S1-S2 | 1.000 | 0.000 | 0.000 | 36.807 | 1.000 | 0.197 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Nb1-Nb3 | 1.000 | 0.000 | 0.000 | 35.748 | 1.000 | 0.102 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.230 | 4.811 | 4.811 | 4.811 |
| or | 2.600 | 83.129 | 79.990 | 83.129 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Nb-Se | 6.942 | 1.138 | 22.849 | 0.0 | 3.460 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 34.409 | 83.129 | 1.138 | 1.138 | 0.0 | 3.460 | 0.0 | 3.460 | 0.0 | 4.127 | |
| 34.973 | 79.990 | 1.138 | 1.138 | 0.0 | 3.460 | 0.0 | 3.460 | 0.0 | 4.127 | |
| 34.409 | 83.129 | 1.138 | 1.138 | 0.0 | 3.460 | 0.0 | 3.460 | 0.0 | 4.127 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nb1-Se1-Se1 | 1.000 | 1.138 | 3.041 | 0.000 | 1.000 | 0.000 | 6.942 | 13.631 | 4 | 0 | 0.0 |
| Nb1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 34.409 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Nb1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 34.973 | 1.000 | 0.174 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Nb1-Nb3 | 1.000 | 0.000 | 0.000 | 34.409 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 14.622 | 8.410 | 8.410 | 8.410 |
| or | 2.000 | 88.054 | 73.258 | 88.054 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-O | 8.317 | 1.015 | 8.000 | 0.0 | 2.712 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 72.735 | 88.054 | 1.015 | 1.015 | 0.0 | 2.712 | 0.0 | 2.712 | 0.0 | 3.222 | |
| 79.226 | 73.258 | 1.015 | 1.015 | 0.0 | 2.712 | 0.0 | 2.712 | 0.0 | 3.222 | |
| 72.735 | 88.054 | 1.015 | 1.015 | 0.0 | 2.712 | 0.0 | 2.712 | 0.0 | 3.222 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo1-O1-O1 | 1.000 | 1.015 | 2.673 | 0.000 | 1.000 | 0.000 | 8.317 | 7.541 | 4 | 0 | 0.0 |
| Mo1-O1-O3 | 1.000 | 0.000 | 0.000 | 72.735 | 1.000 | 0.034 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Mo1-O1-O2 | 1.000 | 0.000 | 0.000 | 79.226 | 1.000 | 0.288 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Mo1-Mo3 | 1.000 | 0.000 | 0.000 | 72.735 | 1.000 | 0.034 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 8.640 | 5.316 | 4.891 |
| or | 2.382 | 80.581 | 80.581 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 6.918 | 1.252 | 17.771 | 0.0 | 3.16 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 67.883 | 81.788 | 1.252 | 1.252 | 0.0 | 3.16 | 0.0 | 3.16 | 0.0 | 3.78 | |
| 62.449 | 81.788 | 1.252 | 1.252 | 0.0 | 3.16 | 0.0 | 3.16 | 0.0 | 4.27 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo1-S1-S1 | 1.000 | 1.252 | 2.523 | 0.000 | 1.000 | 0.000 | 6.918 | 7.223 | 4 | 0 | 0.0 |
| Mo1-S1-S3 | 1.000 | 0.000 | 0.000 | 67.883 | 1.000 | 0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Mo1-Mo3 | 1.000 | 0.000 | 0.000 | 62.449 | 1.000 | 0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 7.928 | 6.945 | 6.945 | 5.782 |
| or | 2.528 | 82.119 | 81.343 | 82.119 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-Se | 5.737 | 0.913 | 18.787 | 0.0 | 3.351 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.526 | 82.119 | 0.913 | 0.913 | 0.0 | 3.351 | 0.0 | 3.351 | 0.0 | 4.000 | |
| 32.654 | 81.343 | 0.913 | 0.913 | 0.0 | 3.351 | 0.0 | 3.351 | 0.0 | 4.000 | |
| 27.079 | 82.119 | 0.913 | 0.913 | 0.0 | 3.351 | 0.0 | 3.351 | 0.0 | 4.000 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo1-Se1-Se1 | 1.000 | 0.913 | 3.672 | 0.000 | 1.000 | 0.000 | 5.737 | 27.084 | 4 | 0 | 0.0 |
| Mo1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 32.526 | 1.000 | 0.137 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Mo1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 32.654 | 1.000 | 0.151 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Mo1-Mo3 | 1.000 | 0.000 | 0.000 | 27.079 | 1.000 | 0.137 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 6.317 | 6.184 | 6.184 | 5.225 |
| or | 2.730 | 81.111 | 82.686 | 81.111 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-Te | 5.086 | 0.880 | 24.440 | 0.0 | 3.604 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 23.705 | 81.111 | 0.880 | 0.880 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 | |
| 23.520 | 82.686 | 0.880 | 0.880 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 | |
| 20.029 | 81.111 | 0.880 | 0.880 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo1-Te1-Te1 | 1.000 | 0.900 | 4.016 | 0.000 | 1.000 | 0.000 | 5.169 | 37.250 | 4 | 0 | 0.0 |
| Mo1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 24.163 | 1.000 | 0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Mo1-Mo3 | 1.000 | 0.000 | 0.000 | 20.416 | 1.000 | 0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.230 | 4.811 | 4.811 | 4.811 |
| or | 2.480 | 83.879 | 78.979 | 83.879 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ta-S | 6.446 | 1.111 | 18.914 | 0.0 | 3.310 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 35.396 | 83.879 | 1.111 | 1.111 | 0.0 | 3.310 | 0.0 | 3.310 | 0.0 | 3.945 | |
| 36.321 | 78.979 | 1.111 | 1.111 | 0.0 | 3.310 | 0.0 | 3.310 | 0.0 | 3.945 | |
| 35.396 | 83.879 | 1.111 | 1.111 | 0.0 | 3.310 | 0.0 | 3.310 | 0.0 | 3.945 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ta1-S1-S1 | 1.000 | 1.111 | 2.979 | 0.000 | 1.000 | 0.000 | 6.446 | 12.408 | 4 | 0 | 0.0 |
| Ta1-S1-S3 | 1.000 | 0.000 | 0.000 | 35.396 | 1.000 | 0.107 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ta1-S1-S2 | 1.000 | 0.000 | 0.000 | 36.321 | 1.000 | 0.191 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Ta1-Ta3 | 1.000 | 0.000 | 0.000 | 35.396 | 1.000 | 0.107 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.230 | 4.811 | 4.811 | 4.811 |
| or | 2.590 | 83.107 | 80.019 | 83.107 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ta-Se | 6.885 | 1.133 | 22.499 | 0.0 | 3.446 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 34.381 | 83.107 | 1.133 | 1.133 | 0.0 | 3.446 | 0.0 | 3.446 | 0.0 | 4.111 | |
| 34.936 | 80.019 | 1.133 | 1.133 | 0.0 | 3.446 | 0.0 | 3.446 | 0.0 | 4.111 | |
| 34.381 | 83.107 | 1.133 | 1.133 | 0.0 | 3.446 | 0.0 | 3.446 | 0.0 | 4.111 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ta1-Se1-Se1 | 1.000 | 1.133 | 3.043 | 0.000 | 1.000 | 0.000 | 6.885 | 13.668 | 4 | 0 | 0.0 |
| Ta1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 34.381 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Ta1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 34.936 | 1.000 | 0.173 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Ta1-Ta3 | 1.000 | 0.000 | 0.000 | 34.381 | 1.000 | 0.120 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 15.318 | 10.276 | 10.276 | 10.276 |
| or | 2.030 | 87.206 | 74.435 | 87.206 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-O | 8.781 | 1.005 | 8.491 | 0.0 | 2.744 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 85.955 | 87.206 | 1.005 | 1.005 | 0.0 | 2.744 | 0.0 | 2.744 | 0.0 | 3.262 | |
| 92.404 | 74.435 | 1.005 | 1.005 | 0.0 | 2.744 | 0.0 | 2.744 | 0.0 | 3.262 | |
| 85.955 | 87.206 | 1.005 | 1.005 | 0.0 | 2.744 | 0.0 | 2.744 | 0.0 | 3.262 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W1-O1-O1 | 1.000 | 1.005 | 2.730 | 0.000 | 1.000 | 0.000 | 8.781 | 8.316 | 4 | 0 | 0.0 |
| W1-O1-O3 | 1.000 | 0.000 | 0.000 | 85.955 | 1.000 | 0.049 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| W1-O1-O2 | 1.000 | 0.000 | 0.000 | 92.404 | 1.000 | 0.268 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-W1-W3 | 1.000 | 0.000 | 0.000 | 85.955 | 1.000 | 0.049 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.701 | 7.421 | 7.421 | 6.607 |
| or | 2.390 | 81.811 | 81.755 | 81.811 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-S | 5.664 | 0.889 | 15.335 | 0.0 | 3.164 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 37.687 | 81.811 | 0.889 | 0.889 | 0.0 | 3.164 | 0.0 | 3.164 | 0.0 | 3.778 | |
| 37.697 | 81.755 | 0.889 | 0.889 | 0.0 | 3.164 | 0.0 | 3.164 | 0.0 | 3.778 | |
| 33.553 | 81.811 | 0.889 | 0.889 | 0.0 | 3.164 | 0.0 | 3.164 | 0.0 | 3.778 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W1-S1-S1 | 1.000 | 0.889 | 3.558 | 0.000 | 1.000 | 0.000 | 5.664 | 24.525 | 4 | 0 | 0.0 |
| W1-S1-S3 | 1.000 | 0.000 | 0.000 | 37.687 | 1.000 | 0.142 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| W1-S1-S2 | 1.000 | 0.000 | 0.000 | 37.697 | 1.000 | 0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-W1-W3 | 1.000 | 0.000 | 0.000 | 33.553 | 1.000 | 0.142 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.286 | 8.513 | 8.513 | 7.719 |
| or | 2.510 | 80.693 | 83.140 | 80.693 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-Se | 5.476 | 0.706 | 16.273 | 0.0 | 3.308 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 25.607 | 80.693 | 0.706 | 0.706 | 0.0 | 3.308 | 0.0 | 3.308 | 0.0 | 3.953 | |
| 25.287 | 83.240 | 0.706 | 0.706 | 0.0 | 3.308 | 0.0 | 3.308 | 0.0 | 3.953 | |
| 23.218 | 80.693 | 0.706 | 0.706 | 0.0 | 3.308 | 0.0 | 3.308 | 0.0 | 3.953 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W1-Se1-Se1 | 1.000 | 0.706 | 4.689 | 0.000 | 1.000 | 0.000 | 5.476 | 65.662 | 4 | 0 | 0.0 |
| W1-Se1-Se3 | 1.000 | 0.000 | 0.000 | 25.607 | 1.000 | 0.162 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| W1-Se1-Se2 | 1.000 | 0.000 | 0.000 | 25.287 | 1.000 | 0.118 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-W1-W3 | 1.000 | 0.000 | 0.000 | 23.218 | 1.000 | 0.162 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 5.483 | 7.016 | 7.016 | 5.718 |
| or | 2.730 | 81.111 | 82.686 | 81.111 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-Te | 4.326 | 0.778 | 22.774 | 0.0 | 3.604 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 21.313 | 81.111 | 0.778 | 0.778 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 | |
| 21.147 | 82.686 | 0.778 | 0.778 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 | |
| 17.370 | 81.111 | 0.778 | 0.778 | 0.0 | 3.604 | 0.0 | 3.604 | 0.0 | 4.305 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W1-Te1-Te1 | 1.000 | 0.778 | 4.632 | 0.000 | 1.000 | 0.000 | 4.326 | 62.148 | 4 | 0 | 0.0 |
| W1-Te1-Te3 | 1.000 | 0.000 | 0.000 | 21.313 | 1.000 | 0.155 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| W1-Te1-Te2 | 1.000 | 0.000 | 0.000 | 21.147 | 1.000 | 0.127 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-W1-W3 | 1.000 | 0.000 | 0.000 | 17.370 | 1.000 | 0.155 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 11.926 | 3.258 | 3.258 |
| or | 2.07 | 102.115 | 102.115 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-O | 10.187 | 1.493 | 9.180 | 0.0 | 2.949 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 50.913 | 102.115 | 1.493 | 1.493 | 0.0 | 2.949 | 0.0 | 2.949 | 0.0 | 4.399 | |
| 50.913 | 102.115 | 1.493 | 1.493 | 0.0 | 2.949 | 0.0 | 2.949 | 0.0 | 4.399 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc-O1-O1 | 1.000 | 1.493 | 1.975 | 50.913 | 1.000 | -0.210 | 10.187 | 1.847 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.512 | 1.593 | 1.593 |
| or | 2.50 | 92.771 | 92.771 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-S | 3.516 | 1.443 | 19.531 | 0.0 | 3.450 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 16.674 | 92.771 | 1.443 | 1.443 | 0.0 | 3.450 | 0.0 | 3.450 | 0.0 | 4.945 | |
| 16.674 | 92.771 | 1.443 | 1.443 | 0.0 | 3.450 | 0.0 | 3.450 | 0.0 | 4.945 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc-S1-S1 | 1.000 | 1.443 | 2.390 | 16.674 | 1.000 | -0.048 | 3.516 | 4.504 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.407 | 2.399 | 2.399 |
| or | 2.64 | 83.621 | 83.621 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-Se | 3.884 | 1.173 | 24.288 | 0.0 | 3.520 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 17.479 | 83.621 | 1.173 | 1.173 | 0.0 | 3.520 | 0.0 | 3.520 | 0.0 | 4.808 | |
| 17.479 | 83.621 | 1.173 | 1.173 | 0.0 | 3.520 | 0.0 | 3.520 | 0.0 | 4.808 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc-Se1-Se1 | 1.000 | 1.173 | 3.000 | 17.479 | 1.000 | 0.111 | 3.884 | 12.814 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.407 | 2.399 | 2.399 |
| or | 2.85 | 81.481 | 81.481 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sc-Te | 4.269 | 1.183 | 32.988 | 0.0 | 3.768 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 16.139 | 81.481 | 1.183 | 1.183 | 0.0 | 3.768 | 0.0 | 3.768 | 0.0 | 5.082 | |
| 16.139 | 81.481 | 1.183 | 1.183 | 0.0 | 3.768 | 0.0 | 3.768 | 0.0 | 5.082 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sc-Te1-Te1 | 1.000 | 1.183 | 3.185 | 16.139 | 1.000 | 0.148 | 4.269 | 16.841 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 9.815 | 3.754 | 3.754 |
| or | 2.390 | 87.984 | 87.984 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ti-S | 7.958 | 1.210 | 16.314 | 0.0 | 3.240 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.377 | 87.984 | 1.210 | 1.210 | 0.0 | 3.240 | 0.0 | 3.240 | 0.0 | 4.535 | |
| 32.377 | 87.984 | 1.210 | 1.210 | 0.0 | 3.240 | 0.0 | 3.240 | 0.0 | 4.535 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ti-S-S | 1.000 | 1.210 | 2.677 | 32.377 | 1.000 | 0.035 | 7.958 | 7.602 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.712 | 3.363 | 3.363 |
| or | 2.510 | 86.199 | 86.199 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ti-Se | 6.582 | 1.207 | 19.846 | 0.0 | 3.380 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 27.044 | 86.199 | 1.207 | 1.207 | 0.0 | 3.380 | 0.0 | 3.380 | 0.0 | 4.685 | |
| 27.044 | 86.199 | 1.207 | 1.207 | 0.0 | 3.380 | 0.0 | 3.380 | 0.0 | 4.685 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ti-Se-Se | 1.000 | 1.207 | 2.801 | 27.044 | 1.000 | 0.066 | 6.582 | 9.362 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.758 | 3.217 | 3.217 |
| or | 2.730 | 83.621 | 83.621 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ti-Te | 3.542 | 1.213 | 27.773 | 0.0 | 3.640 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 23.439 | 83.621 | 1.213 | 1.213 | 0.0 | 3.640 | 0.0 | 3.640 | 0.0 | 4.972 | |
| 23.439 | 83.621 | 1.213 | 1.213 | 0.0 | 3.640 | 0.0 | 3.640 | 0.0 | 4.972 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ti-Te-Te | 1.000 | 1.213 | 3.000 | 23.439 | 1.000 | 0.111 | 3.542 | 12.814 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 11.562 | 4.237 | 4.237 |
| or | 2.310 | 84.288 | 84.288 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-S | 7.943 | 1.048 | 14.237 | 0.0 | 3.088 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 31.659 | 84.288 | 1.048 | 1.048 | 0.0 | 3.088 | 0.0 | 3.088 | 0.0 | 4.235 | |
| 31.659 | 84.288 | 1.048 | 1.048 | 0.0 | 3.088 | 0.0 | 3.088 | 0.0 | 4.235 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V-S1-S1 | 1.000 | 1.048 | 2.946 | 31.659 | 1.000 | 0.100 | 7.943 | 11.797 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 11.562 | 4.237 | 4.237 |
| or | 2.440 | 83.201 | 83.201 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-Se | 8.606 | 1.070 | 17.723 | 0.0 | 3.248 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.387 | 83.201 | 1.070 | 1.070 | 0.0 | 3.248 | 0.0 | 3.248 | 0.0 | 4.426 | |
| 30.387 | 83.201 | 1.070 | 1.070 | 0.0 | 3.248 | 0.0 | 3.248 | 0.0 | 4.426 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V-Se1-Se1 | 1.000 | 1.070 | 3.035 | 30.387 | 1.000 | 0.118 | 8.606 | 13.507 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 10.476 | 3.814 | 3.814 |
| or | 2.640 | 81.885 | 81.885 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| V-Te | 8.805 | 1.110 | 24.288 | 0.0 | 3.496 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 26.043 | 81.885 | 1.110 | 1.110 | 0.0 | 3.496 | 0.0 | 3.496 | 0.0 | 4.726 | |
| 26.043 | 81.885 | 1.110 | 1.110 | 0.0 | 3.496 | 0.0 | 3.496 | 0.0 | 4.726 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| V-Te1-Te1 | 1.000 | 1.110 | 3.149 | 26.043 | 1.000 | 0.141 | 8.805 | 15.980 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 15.371 | 4.822 | 4.822 |
| or | 1.88 | 97.181 | 97.181 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mn-O | 9.675 | 1.212 | 6.246 | 0.0 | 2.635 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 60.755 | 97.181 | 1.212 | 1.212 | 0.0 | 2.635 | 0.0 | 2.635 | 0.0 | 3.852 | |
| 60.755 | 97.181 | 1.212 | 1.212 | 0.0 | 2.635 | 0.0 | 2.635 | 0.0 | 3.852 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mn-O1-O1 | 1.000 | 1.212 | 2.175 | 60.755 | 1.000 | -0.125 | 9.675 | 2.899 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.407 | 2.399 | 2.399 |
| or | 2.27 | 86.822 | 86.822 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mn-S | 3.127 | 1.111 | 13.276 | 0.0 | 3.064 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 19.765 | 86.822 | 1.111 | 1.111 | 0.0 | 3.064 | 0.0 | 3.064 | 0.0 | 4.262 | |
| 19.765 | 86.822 | 1.111 | 1.111 | 0.0 | 3.064 | 0.0 | 3.064 | 0.0 | 4.262 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mn-S1-S1 | 1.000 | 1.111 | 2.757 | 19.765 | 1.000 | 0.055 | 3.127 | 8.700 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.407 | 2.399 | 2.399 |
| or | 2.39 | 86.330 | 86.330 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mn-Se | 3.422 | 1.153 | 16.314 | 0.0 | 3.220 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 19.390 | 86.330 | 1.153 | 1.153 | 0.0 | 3.220 | 0.0 | 3.220 | 0.0 | 4.467 | |
| 19.390 | 86.330 | 1.153 | 1.153 | 0.0 | 3.220 | 0.0 | 3.220 | 0.0 | 4.467 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mn-Se1-Se1 | 1.000 | 1.153 | 2.792 | 19.390 | 1.000 | 0.064 | 3.422 | 9.219 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.407 | 2.399 | 2.399 |
| or | 2.59 | 86.219 | 86.219 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mn-Te | 4.007 | 1.246 | 22.499 | 0.0 | 3.488 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 19.307 | 86.219 | 1.246 | 1.246 | 0.0 | 3.488 | 0.0 | 3.488 | 0.0 | 4.836 | |
| 19.307 | 86.219 | 1.246 | 1.246 | 0.0 | 3.488 | 0.0 | 3.488 | 0.0 | 4.836 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mn-Te1-Te1 | 1.000 | 1.246 | 2.800 | 19.307 | 1.000 | 0.066 | 4.007 | 9.340 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.726 | 3.035 | 3.035 |
| or | 2.512 | 91.501 | 91.501 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Co-Te | 4.628 | 1.402 | 19.899 | 0.0 | 3.450 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.149 | 91.501 | 1.402 | 1.402 | 0.0 | 3.450 | 0.0 | 3.450 | 0.0 | 4.915 | |
| 30.149 | 91.501 | 1.402 | 1.402 | 0.0 | 3.450 | 0.0 | 3.450 | 0.0 | 4.915 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Co-Te1-Te1 | 1.000 | 1.402 | 2.461 | 30.149 | 1.000 | -0.026 | 4.628 | 5.151 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 15.925 | 4.847 | 4.847 |
| or | 97.653 | 97.653 | |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-O | 9.709 | 1.199 | 5.731 | 0.0 | 2.583 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 62.317 | 97.653 | 1.199 | 1.199 | 0.0 | 2.583 | 0.0 | 2.583 | 0.0 | 3.784 | |
| 62.317 | 97.653 | 1.199 | 1.199 | 0.0 | 2.583 | 0.0 | 2.583 | 0.0 | 3.784 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni-O1-O1 | 1.000 | 1.199 | 2.154 | 62.317 | 1.000 | -0.133 | 9.709 | 2.772 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 9.385 | 2.952 | 2.952 |
| or | 2.232 | 96.000 | 96.000 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-S | 8.098 | 1.398 | 12.409 | 0.0 | 3.115 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 35.372 | 96.000 | 1.398 | 1.398 | 0.0 | 3.115 | 0.0 | 3.115 | 0.0 | 4.532 | |
| 35.372 | 96.000 | 1.398 | 1.398 | 0.0 | 3.115 | 0.0 | 3.115 | 0.0 | 4.532 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni-S1-S1 | 1.000 | 1.398 | 2.228 | 35.372 | 1.000 | -0.105 | 8.098 | 3.249 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 8.814 | 3.149 | 3.149 |
| or | 2.339 | 95.798 | 95.798 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-Se | 8.313 | 1.458 | 14.971 | 0.0 | 3.263 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 37.407 | 95.798 | 1.458 | 1.458 | 0.0 | 3.263 | 0.0 | 3.263 | 0.0 | 4.742 | |
| 37.407 | 95.798 | 1.458 | 1.458 | 0.0 | 3.263 | 0.0 | 3.263 | 0.0 | 4.742 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni-Se1-Se1 | 1.000 | 1.458 | 2.238 | 37.407 | 1.000 | -0.101 | 8.313 | 3.315 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.230 | 2.429 | 2.429 |
| or | 2.532 | 94.702 | 94.702 |
| or | 2.635 | 95.999 | 95.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ni-Te | 4.554 | 1.536 | 20.554 | 0.0 | 3.518 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 27.553 | 94.702 | 1.536 | 1.536 | 0.0 | 3.518 | 0.0 | 3.518 | 0.0 | 5.088 | |
| 27.553 | 94.702 | 1.536 | 1.536 | 0.0 | 3.518 | 0.0 | 3.518 | 0.0 | 5.088 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ni-Te1-Te1 | 1.000 | 1.536 | 2.291 | 27.553 | 1.000 | -0.082 | 4.554 | 3.696 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.580 | 91.305 | 91.305 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Zr-S | 8.149 | 1.432 | 22.154 | 0.0 | 3.541 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 42.170 | 91.305 | 1.432 | 1.432 | 0.0 | 3.541 | 0.0 | 3.541 | 0.0 | 5.041 | |
| 42.170 | 91.305 | 1.432 | 1.432 | 0.0 | 3.541 | 0.0 | 3.541 | 0.0 | 5.041 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Zr-S1-S1 | 1.000 | 1.432 | 2.473 | 42.177 | 1.000 | -0.023 | 8.149 | 5.268 | 4 | 0 | 0.0 |
| S1-Zr-Zr | 1.000 | 1.432 | 2.473 | 42.177 | 1.000 | -0.023 | 8.149 | 5.268 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.667 | 88.058 | 88.058 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Zr-Se | 8.022 | 1.354 | 25.297 | 0.0 | 3.617 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 37.051 | 88.058 | 1.354 | 1.354 | 0.0 | 3.617 | 0.0 | 3.617 | 0.0 | 5.064 | |
| 37.051 | 88.058 | 1.354 | 1.354 | 0.0 | 3.617 | 0.0 | 3.617 | 0.0 | 5.064 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Zr-Se-Se | 1.000 | 1.354 | 2.671 | 37.051 | 1.000 | 0.034 | 8.022 | 7.527 | 4 | 0 | 0.0 |
| Se-Zr-Zr | 1.000 | 1.354 | 2.671 | 37.051 | 1.000 | 0.034 | 8.022 | 7.527 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.974 | 3.681 | 3.681 |
| or | 2.902 | 87.301 | 87.301 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Zr-Te | 3.493 | 1.441 | 35.467 | 0.0 | 3.925 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.905 | 87.301 | 1.441 | 1.441 | 0.0 | 3.925 | 0.0 | 3.925 | 0.0 | 5.473 | |
| 30.905 | 87.301 | 1.441 | 1.441 | 0.0 | 3.925 | 0.0 | 3.925 | 0.0 | 5.473 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Zr-Te1-Te1 | 1.000 | 1.441 | 2.723 | 30.905 | 1.000 | 0.047 | 3.493 | 8.225 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.450 | 84.671 | 84.671 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Nb-S | 6.192 | 1.125 | 18.015 | 0.0 | 3.280 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.472 | 84.671 | 1.125 | 1.125 | 0.0 | 3.280 | 0.0 | 3.280 | 0.0 | 4.508 | |
| 32.472 | 84.671 | 1.125 | 1.125 | 0.0 | 3.280 | 0.0 | 3.280 | 0.0 | 4.508 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nb-S1-S1 | 1.000 | 1.125 | 2.916 | 32.472 | 1.000 | 0.093 | 6.192 | 11.247 | 4 | 0 | 0.0 |
| S1-Nb-Nb | 1.000 | 1.125 | 2.916 | 32.472 | 1.000 | 0.093 | 6.192 | 11.247 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.570 | 82.529 | 82.529 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Nb-Se | 6.430 | 1.104 | 21.812 | 0.0 | 3.412 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 29.956 | 82.528 | 1.104 | 1.104 | 0.0 | 3.412 | 0.0 | 3.412 | 0.0 | 4.631 | |
| 29.956 | 82.528 | 1.104 | 1.104 | 0.0 | 3.412 | 0.0 | 3.412 | 0.0 | 4.631 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nb-Se1-Se1 | 1.000 | 1.104 | 3.092 | 29.956 | 1.000 | 0.130 | 6.430 | 14.706 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.559 | 4.863 | 4.863 |
| or | 2.770 | 79.972 | 79.972 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Nb-Te | 3.123 | 1.094 | 29.437 | 0.0 | 3.640 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 30.968 | 79.972 | 1.094 | 1.094 | 0.0 | 3.640 | 0.0 | 3.640 | 0.0 | 4.863 | |
| 30.968 | 79.972 | 1.094 | 1.094 | 0.0 | 3.640 | 0.0 | 3.640 | 0.0 | 4.863 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nb-Te1-Te1 | 1.000 | 1.094 | 3.328 | 30.968 | 1.000 | 0.174 | 3.123 | 20.560 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.523 | 10.394 | 10.394 |
| or | 2.419 | 82.799 | 82.799 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-S | 2.550 | 1.048 | 17.129 | 0.0 | 3.215 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 73.436 | 82.799 | 1.048 | 1.048 | 0.0 | 3.215 | 0.0 | 3.215 | 0.0 | 4.371 | |
| 73.436 | 82.799 | 1.048 | 1.048 | 0.0 | 3.215 | 0.0 | 3.215 | 0.0 | 4.371 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo-S1-S1 | 1.000 | 1.048 | 3.069 | 73.436 | 1.000 | 0.125 | 2.550 | 14.207 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.964 | 14.753 | 14.753 |
| or | 2.529 | 80.501 | 80.501 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-Se | 2.201 | 1.017 | 20.463 | 0.0 | 3.331 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 95.770 | 80.501 | 1.017 | 1.017 | 0.0 | 3.331 | 0.0 | 3.331 | 0.0 | 4.465 | |
| 95.770 | 80.501 | 1.017 | 1.017 | 0.0 | 3.331 | 0.0 | 3.331 | 0.0 | 4.465 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo-Se1-Se1 | 1.000 | 1.017 | 3.276 | 95.770 | 1.000 | 0.165 | 2.201 | 19.152 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.074 | 12.516 | 12.516 |
| or | 2.729 | 79.700 | 79.700 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Mo-Te | 2.597 | 1.068 | 27.720 | 0.0 | 3.582 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 78.925 | 79.700 | 1.068 | 1.068 | 0.0 | 3.582 | 0.0 | 3.582 | 0.0 | 4.777 | |
| 78.925 | 79.700 | 1.068 | 1.068 | 0.0 | 3.582 | 0.0 | 3.582 | 0.0 | 4.777 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mo-Te1-Te1 | 1.000 | 1.068 | 3.355 | 78.925 | 1.000 | 0.179 | 2.597 | 21.328 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.986 | 11.141 | 11.141 |
| or | 2.392 | 79.800 | 79.800 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Tc-S | 1.945 | 0.939 | 16.380 | 0.0 | 3.142 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 70.512 | 79.800 | 0.939 | 0.939 | 0.0 | 3.142 | 0.0 | 3.142 | 0.0 | 4.193 | |
| 70.512 | 79.800 | 0.939 | 0.939 | 0.0 | 3.142 | 0.0 | 3.142 | 0.0 | 4.193 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Tc-S1-S1 | 1.000 | 0.939 | 3.345 | 70.512 | 1.000 | 0.177 | 1.945 | 21.038 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.467 | 10.636 | 10.636 |
| or | 2.506 | 78.001 | 78.001 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Tc-Se | 2.355 | 0.925 | 19.723 | 0.0 | 3.267 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 63.150 | 78.001 | 0.925 | 0.925 | 0.0 | 3.267 | 0.0 | 3.267 | 0.0 | 4.309 | |
| 63.150 | 78.001 | 0.925 | 0.925 | 0.0 | 3.267 | 0.0 | 3.267 | 0.0 | 4.309 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Tc-Se1-Se1 | 1.000 | 0.925 | 3.532 | 63.150 | 1.000 | 0.208 | 2.355 | 26.932 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 0.785 | 8.894 | 8.894 |
| or | 2.690 | 78.801 | 78.801 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Tc-Te | 0.628 | 1.021 | 26.181 | 0.0 | 3.519 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 54.313 | 78.801 | 1.021 | 1.021 | 0.0 | 3.519 | 0.0 | 3.519 | 0.0 | 4.665 | |
| 54.313 | 78.801 | 1.021 | 1.021 | 0.0 | 3.519 | 0.0 | 3.519 | 0.0 | 4.665 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Tc-Te1-Te1 | 1.000 | 1.021 | 3.447 | 54.313 | 1.000 | 0.194 | 0.628 | 24.110 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.366 | 1.869 | 1.869 |
| or | 2.633 | 91.001 | 91.001 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Rh-Te | 4.640 | 1.450 | 24.038 | 0.0 | 3.610 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 18.192 | 91.001 | 1.450 | 1.450 | 0.0 | 3.610 | 0.0 | 3.610 | 0.0 | 5.131 | |
| 18.192 | 91.001 | 1.450 | 1.450 | 0.0 | 3.610 | 0.0 | 3.610 | 0.0 | 5.131 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Rh-Te1-Te1 | 1.000 | 1.450 | 2.490 | 18.192 | 1.000 | -0.017 | 4.640 | 5.436 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 10.374 | 3.122 | 3.122 |
| or | 2.401 | 94.998 | 94.998 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pd-S | 10.116 | 1.467 | 16.625 | 0.0 | 3.340 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 35.859 | 94.998 | 1.467 | 1.467 | 0.0 | 3.340 | 0.0 | 3.340 | 0.0 | 4.837 | |
| 35.859 | 94.998 | 1.467 | 1.467 | 0.0 | 3.340 | 0.0 | 3.340 | 0.0 | 4.837 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pd-S1-S1 | 1.000 | 1.467 | 2.276 | 35.859 | 1.000 | -0.087 | 10.116 | 3.588 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 10.374 | 3.122 | 3.122 |
| or | 2.493 | 94.999 | 94.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pd-Se | 10.902 | 1.523 | 19.310 | 0.0 | 3.467 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 35.859 | 94.999 | 1.523 | 1.523 | 0.0 | 3.467 | 0.0 | 3.467 | 0.0 | 5.021 | |
| 35.859 | 94.999 | 1.523 | 1.523 | 0.0 | 3.467 | 0.0 | 3.467 | 0.0 | 5.021 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pd-Se1-Se1 | 1.000 | 1.523 | 2.276 | 35.859 | 1.000 | -0.087 | 10.902 | 3.588 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 10.374 | 3.122 | 3.122 |
| or | 2.635 | 95.999 | 95.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pd-Te | 12.474 | 1.650 | 24.101 | 0.0 | 3.678 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 37.406 | 95.999 | 1.650 | 1.650 | 0.0 | 3.678 | 0.0 | 3.678 | 0.0 | 5.350 | |
| 37.406 | 95.999 | 1.650 | 1.650 | 0.0 | 3.678 | 0.0 | 3.678 | 0.0 | 5.350 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pd-Te1-Te1 | 1.000 | 1.650 | 2.229 | 37.406 | 1.000 | -0.105 | 12.474 | 3.250 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.872 | 5.817 | 5.817 |
| or | 2.570 | 90.173 | 90.173 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-S | 7.805 | 1.384 | 21.812 | 0.0 | 3.513 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 54.748 | 90.173 | 1.384 | 1.384 | 0.0 | 3.513 | 0.0 | 3.513 | 0.0 | 4.972 | |
| 54.748 | 90.173 | 1.384 | 1.384 | 0.0 | 3.513 | 0.0 | 3.513 | 0.0 | 4.972 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-S1-S1 | 1.000 | 1.384 | 2.539 | 54.748 | 1.000 | -0.003 | 7.805 | 5.949 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.872 | 5.817 | 5.817 |
| or | 2.704 | 89.044 | 89.044 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-Se | 8.395 | 1.411 | 26.730 | 0.0 | 3.681 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 52.322 | 89.044 | 1.411 | 1.411 | 0.0 | 3.681 | 0.0 | 3.681 | 0.0 | 5.180 | |
| 52.322 | 89.044 | 1.411 | 1.411 | 0.0 | 3.681 | 0.0 | 3.681 | 0.0 | 5.180 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Se1-Se1 | 1.000 | 1.411 | 2.609 | 52.322 | 1.000 | 0.017 | 8.395 | 6.743 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.550 | 91.078 | 91.078 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Hf-S | 7.917 | 1.407 | 21.141 | 0.0 | 3.497 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 41.798 | 91.078 | 1.407 | 1.407 | 0.0 | 3.497 | 0.0 | 3.497 | 0.0 | 4.973 | |
| 41.798 | 91.078 | 1.407 | 1.407 | 0.0 | 3.497 | 0.0 | 3.497 | 0.0 | 4.973 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Hf-S-S | 1.000 | 1.407 | 2.485 | 41.798 | 1.000 | -0.019 | 7.917 | 5.394 | 4 | 0 | 0.0 |
| S-Hf-Hf | 1.000 | 1.407 | 2.485 | 41.798 | 1.000 | -0.019 | 7.917 | 5.394 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 7.930 | 4.283 | 4.283 |
| or | 2.642 | 88.093 | 88.093 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Hf-Se | 7.871 | 1.341 | 24.361 | 0.0 | 3.583 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 37.039 | 88.093 | 1.341 | 1.341 | 0.0 | 3.583 | 0.0 | 3.583 | 0.0 | 5.018 | |
| 37.039 | 88.093 | 1.341 | 1.341 | 0.0 | 3.583 | 0.0 | 3.583 | 0.0 | 5.018 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Hf-Se-Se | 1.000 | 1.341 | 2.672 | 37.039 | 1.000 | 0.033 | 7.871 | 7.533 | 4 | 0 | 0.0 |
| Se-Hf-Hf | 1.000 | 1.341 | 2.672 | 37.039 | 1.000 | 0.033 | 7.871 | 7.533 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.328 | 3.877 | 3.877 |
| or | 2.856 | 87.801 | 87.801 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Hf-Te | 3.835 | 1.439 | 33.262 | 0.0 | 3.869 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 33.196 | 87.801 | 1.439 | 1.439 | 0.0 | 3.869 | 0.0 | 3.869 | 0.0 | 5.410 | |
| 33.196 | 87.801 | 1.439 | 1.439 | 0.0 | 3.869 | 0.0 | 3.869 | 0.0 | 5.410 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Hf-Te1-Te1 | 1.000 | 1.439 | 2.690 | 33.196 | 1.000 | 0.038 | 3.835 | 7.764 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 11.192 | 4.774 | 4.774 |
| or | 2.458 | 85.999 | 85.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ta-S | 9.110 | 1.174 | 18.246 | 0.0 | 3.307 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 38.092 | 85.999 | 1.174 | 1.174 | 0.0 | 3.307 | 0.0 | 3.307 | 0.0 | 4.579 | |
| 38.092 | 85.999 | 1.174 | 1.174 | 0.0 | 3.307 | 0.0 | 3.307 | 0.0 | 4.579 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ta-S1-S1 | 1.000 | 1.174 | 2.816 | 38.092 | 1.000 | 0.070 | 9.110 | 9.589 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 9.348 | 4.535 | 4.535 |
| or | 2.561 | 84.999 | 84.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ta-Se | 8.045 | 1.188 | 21.505 | 0.0 | 3.433 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 34.820 | 84.999 | 1.188 | 1.188 | 0.0 | 3.433 | 0.0 | 3.3433 | 0.0 | 4.727 | |
| 34.820 | 84.999 | 1.188 | 1.188 | 0.0 | 3.433 | 0.0 | 3.3433 | 0.0 | 4.727 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ta-Se1-Se1 | 1.000 | 1.188 | 2.891 | 34.820 | 1.000 | 0.087 | 8.045 | 10.813 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 3.442 | 4.516 | 4.516 |
| or | 2.770 | 82.999 | 82.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ta-Te | 3.283 | 1.207 | 29.415 | 0.0 | 3.684 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.144 | 82.999 | 1.207 | 1.207 | 0.0 | 3.684 | 0.0 | 3.684 | 0.0 | 5.014 | |
| 32.144 | 82.999 | 1.207 | 1.207 | 0.0 | 3.684 | 0.0 | 3.684 | 0.0 | 5.014 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ta-Se1-Se1 | 1.000 | 1.188 | 2.891 | 34.820 | 1.000 | 0.087 | 8.045 | 10.813 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.395 | 10.087 | 10.087 |
| or | 2.413 | 82.799 | 82.799 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-S | 3.163 | 1.045 | 16.937 | 0.0 | 3.206 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 71.264 | 82.799 | 1.045 | 1.045 | 0.0 | 3.206 | 0.0 | 3.206 | 0.0 | 4.359 | |
| 71.264 | 82.799 | 1.045 | 1.045 | 0.0 | 3.206 | 0.0 | 3.206 | 0.0 | 4.359 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W-S1-S1 | 1.000 | 1.045 | 3.069 | 71.264 | 1.000 | 0.125 | 3.163 | 14.209 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.556 | 15.375 | 15.375 |
| or | 2.521 | 80.501 | 80.501 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-Se | 1.885 | 1.013 | 20.186 | 0.0 | 3.320 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 99.800 | 80.501 | 1.013 | 1.013 | 0.0 | 3.320 | 0.0 | 3.320 | 0.0 | 4.450 | |
| 99.800 | 80.501 | 1.013 | 1.013 | 0.0 | 3.320 | 0.0 | 3.320 | 0.0 | 4.450 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W-Se1-Se1 | 1.000 | 1.013 | 3.277 | 99.800 | 1.000 | 0.165 | 1.885 | 19.156 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.272 | 19.437 | 19.437 |
| or | 2.720 | 79.999 | 79.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| W-Te | 1.924 | 1.075 | 27.376 | 0.0 | 3.575 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 123.899 | 79.999 | 1.075 | 1.075 | 0.0 | 3.575 | 0.0 | 3.575 | 0.0 | 4.777 | |
| 123.899 | 79.999 | 1.075 | 1.075 | 0.0 | 3.575 | 0.0 | 3.575 | 0.0 | 4.777 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| W-Te1-Te1 | 1.000 | 1.075 | 3.325 | 123.899 | 1.000 | 0.174 | 1.924 | 20.483 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 2.684 | 10.829 | 10.829 |
| or | 2.405 | 79.498 | 79.498 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Re-S | 1.751 | 0.934 | 16.714 | 0.0 | 3.154 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 67.797 | 79.498 | 0.934 | 0.934 | 0.0 | 3.154 | 0.0 | 3.154 | 0.0 | 4.201 | |
| 67.797 | 79.498 | 0.934 | 0.934 | 0.0 | 3.154 | 0.0 | 3.154 | 0.0 | 4.201 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Re-S1-S1 | 1.000 | 0.934 | 3.375 | 67.797 | 1.000 | 0.182 | 1.751 | 21.916 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 4.313 | 12.674 | 12.674 |
| or | 2.515 | 76.999 | 76.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Re-Se | 2.866 | 0.896 | 20.001 | 0.0 | 3.265 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 72.666 | 76.999 | 0.896 | 0.896 | 0.0 | 3.265 | 0.0 | 3.265 | 0.0 | 4.277 | |
| 72.666 | 76.999 | 0.896 | 0.896 | 0.0 | 3.265 | 0.0 | 3.265 | 0.0 | 4.277 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Re-Se1-Se1 | 1.000 | 0.896 | 3.645 | 72.666 | 1.000 | 0.225 | 2.866 | 31.036 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 1.724 | 14.812 | 14.812 |
| or | 2.703 | 77.501 | 77.501 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Re-Te | 1.343 | 0.980 | 26.678 | 0.0 | 3.517 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 86.424 | 77.501 | 0.980 | 0.980 | 0.0 | 3.517 | 0.0 | 3.517 | 0.0 | 4.622 | |
| 86.424 | 77.501 | 0.980 | 0.980 | 0.0 | 3.517 | 0.0 | 3.517 | 0.0 | 4.622 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Re-Te1-Te1 | 1.000 | 0.980 | 3.587 | 86.424 | 1.000 | 0.216 | 1.343 | 28.891 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 5.334 | 2.182 | 2.182 |
| or | 2.649 | 93.002 | 93.002 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ir-Te | 6.030 | 1.538 | 24.621 | 0.0 | 3.658 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 23.056 | 93.002 | 1.538 | 1.538 | 0.0 | 3.658 | 0.0 | 3.658 | 0.0 | 5.250 | |
| 23.056 | 93.002 | 1.538 | 1.538 | 0.0 | 3.658 | 0.0 | 3.658 | 0.0 | 5.250 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ir-Te1-Te1 | 1.000 | 1.538 | 2.370 | 23.056 | 1.000 | -0.052 | 6.030 | 4.398 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 12.128 | 4.975 | 4.975 |
| or | 2.371 | 96.00 | 96.00 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pt-S | 11.806 | 1.485 | 15.796 | 0.0 | 3.309 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 59.607 | 96.00 | 1.485 | 1.485 | 0.0 | 3.309 | 0.0 | 3.309 | 0.0 | 4.813 | |
| 59.607 | 96.00 | 1.485 | 1.485 | 0.0 | 3.309 | 0.0 | 3.309 | 0.0 | 4.813 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pt-S1-S1 | 1.000 | 1.485 | 2.229 | 59.607 | 1.000 | -0.105 | 11.806 | 3.250 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 12.128 | 4.975 | 4.975 |
| or | 2.467 | 95.999 | 95.999 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pt-Se | 12.781 | 1.545 | 18.511 | 0.0 | 3.443 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 59.608 | 95.999 | 1.545 | 1.545 | 0.0 | 3.443 | 0.0 | 3.443 | 0.0 | 5.008 | |
| 59.608 | 95.999 | 1.545 | 1.545 | 0.0 | 3.443 | 0.0 | 3.443 | 0.0 | 5.008 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pt-Se1-Se1 | 1.000 | 1.545 | 2.229 | 59.608 | 1.000 | -0.105 | 12.781 | 3.250 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |
|---|---|---|---|
| expression | |||
| parameter | 12.128 | 4.975 | 4.975 |
| or | 2.661 | 95.998 | 95.998 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Pt-Te | 14.877 | 1.667 | 25.081 | 0.0 | 3.714 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 59.607 | 95.998 | 1.667 | 1.667 | 0.0 | 3.714 | 0.0 | 3.714 | 0.0 | 5.403 | |
| 59.607 | 95.998 | 1.667 | 1.667 | 0.0 | 3.714 | 0.0 | 3.714 | 0.0 | 5.403 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Pt-Te1-Te1 | 1.000 | 1.667 | 2.229 | 59.607 | 1.000 | -0.104 | 14.877 | 3.250 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 10.542 | 10.542 | 7.048 | 7.048 |
| or | 2.238 | 2.260 | 96.581 | 102.307 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 4.172 | 0.551 | 12.543 | 0.0 | 2.793 | |
| 4.976 | 0.685 | 13.044 | 0.0 | 2.882 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 25.965 | 96.581 | 0.551 | 0.551 | 0.0 | 2.793 | 0.0 | 2.793 | 2.793 | 3.365 | |
| 29.932 | 102.307 | 0.551 | 0.685 | 0.0 | 2.793 | 0.0 | 2.882 | 2.882 | 3.772 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| P1-P1-P1 | 1.000 | 0.551 | 5.069 | 25.965 | 1.000 | -0.115 | 4.172 | 136.080 | 4 | 0 | 0.0 |
| P1-P2-P2 | 1.000 | 0.685 | 4.207 | 0.000 | 1.000 | 0.000 | 4.976 | 59.245 | 4 | 0 | 0.0 |
| P1-P1-P2 | 1.000 | 0.000 | 0.000 | 29.932 | 1.000 | -0.213 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 7.936 | 7.936 | 7.456 | 7.456 |
| or | 2.508 | 2.495 | 94.400 | 100.692 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 3.180 | 0.455 | 19.782 | 0.0 | 3.042 | |
| 4.477 | 0.737 | 19.375 | 0.0 | 3.173 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 20.597 | 94.400 | 0.455 | 0.455 | 0.0 | 3.042 | 0.0 | 3.042 | 3.628 | 4.225 | |
| 26.831 | 100.692 | 0.455 | 0.737 | 0.0 | 3.042 | 0.0 | 3.173 | 3.173 | 4.149 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| As1-As1-As1 | 1.000 | 0.455 | 6.686 | 20.597 | 1.000 | -0.077 | 3.180 | 461.556 | 4 | 0 | 0.0 |
| As1-As2-As2 | 1.000 | 0.737 | 4.305 | 0.000 | 1.000 | 0.000 | 4.477 | 65.671 | 4 | 0 | 0.0 |
| As1-As1-As2 | 1.000 | 0.000 | 0.000 | 26.831 | 1.000 | -0.186 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.675 | 7.675 | 6.534 | 12.068 | 12.068 |
| or | 2.950 | 2.870 | 95.380 | 88.300 | 102.800 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 1.750 | 0.122 | 37.867 | 0.0 | 3.250 | |
| 11.221 | 1.843 | 33.923 | 0.0 | 4.020 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 7.435 | 95.380 | 0.122 | 0.122 | 0.0 | 3.250 | 0.0 | 3.250 | 0.0 | 4.545 | |
| 45.054 | 88.380 | 1.843 | 0.122 | 0.0 | 4.020 | 0.0 | 3.250 | 0.0 | 5.715 | |
| 47.338 | 102.800 | 1.843 | 0.122 | 0.0 | 4.020 | 0.0 | 3.250 | 0.0 | 6.105 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sb5-Sb4-Sb4 | 1.000 | 5.103 | 0.958 | 635.059 | 1.000 | -0.094 | 38.498 | 0.056 | 4 | 0 | 0.0 |
| Sb1-Sb2-Sb2 | 1.000 | 1.924 | 2.102 | 0.000 | 1.000 | 0.000 | 11.708 | 2.476 | 4 | 0 | 0.0 |
| Sb5-Sb4-Sb6 | 1.000 | 0.000 | 0.000 | 431.139 | 1.000 | 0.030 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Sb2-Sb3-Sb1 | 1.000 | 0.000 | 0.000 | 452.994 | 1.000 | -0.222 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.675 | 7.675 | 2.267 | 8.347 | 8.347 |
| or | 3.110 | 3.097 | 94.018 | 86.486 | 103.491 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 1.777 | 0.109 | 46.775 | 0.0 | 3.401 | |
| 12.322 | 1.872 | 45.998 | 0.0 | 4.301 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 2.408 | 94.018 | 0.109 | 0.109 | 0.0 | 3.401 | 0.0 | 3.401 | 0.0 | 4.745 | |
| 28.842 | 86.486 | 1.872 | 0.109 | 0.0 | 4.301 | 0.0 | 3.401 | 0.0 | 5.982 | |
| 30.388 | 103.491 | 1.872 | 0.109 | 0.0 | 4.301 | 0.0 | 3.401 | 0.0 | 6.473 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Bi1-Bi8-Bi8 | 1.000 | 2.737 | 1.571 | 112.813 | 1.000 | -0.070 | 18.974 | 1.000 | 4 | 0 | 0.0 |
| Bi1-Bi2-Bi2 | 1.000 | 2.808 | 1.532 | 0.000 | 1.000 | 0.000 | 19.577 | 0.888 | 4 | 0 | 0.0 |
| Bi1-Bi8-Bi2 | 1.000 | 0.000 | 0.000 | 429.598 | 1.000 | 0.061 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Bi2-Bi3-Bi1 | 1.000 | 0.000 | 0.000 | 452.618 | 1.000 | -0.233 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 12.191 | 12.191 | 4.817 | 3.123 | 3.123 |
| or | 1.843 | 1.859 | 95.989 | 96.000 | 132.005 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 19.127 | 2.720 | 5.769 | 0.0 | 2.962 | |
| 7.105 | 1.133 | 5.972 | 0.0 | 2.585 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 314.008 | 95.989 | 2.720 | 2.720 | 0.0 | 2.962 | 0.0 | 2.962 | 0.0 | 3.720 | |
| 85.406 | 96.000 | 1.133 | 2.720 | 0.0 | 2.585 | 0.0 | 2.962 | 0.0 | 3.875 | |
| 152.982 | 132.005 | 1.133 | 2.720 | 0.0 | 2.585 | 0.0 | 2.962 | 0.0 | 4.194 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si1-O2-O2 | 1.000 | 2.720 | 1.089 | 314.008 | 1.000 | -0.104 | 19.127 | 0.105 | 4 | 0 | 0.0 |
| Si1-O1-O1 | 1.000 | 1.133 | 2.282 | 0.000 | 1.000 | 0.000 | 7.105 | 3.630 | 4 | 0 | 0.0 |
| Si1-O1-O2 | 1.000 | 0.000 | 0.000 | 85.406 | 1.000 | -0.105 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Si1-Si2 | 1.000 | 0.000 | 0.000 | 152.982 | 1.000 | -0.669 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 12.191 | 12.191 | 4.817 | 3.123 | 3.123 |
| or | 1.956 | 1.986 | 102.692 | 93.300 | 128.213 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 21.562 | 2.889 | 7.319 | 0.0 | 3.144 | |
| 9.258 | 1.384 | 7.778 | 0.0 | 2.815 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 326.824 | 102.692 | 2.889 | 2.889 | 0.0 | 3.144 | 0.0 | 3.144 | 0.0 | 3.928 | |
| 94.550 | 93.300 | 1.384 | 2.889 | 0.0 | 2.815 | 0.0 | 3.144 | 0.0 | 3.933 | |
| 152.646 | 128.213 | 1.384 | 2.889 | 0.0 | 2.815 | 0.0 | 3.144 | 0.0 | 4.284 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge1-O2-O2 | 1.000 | 2.889 | 1.089 | 326.824 | 1.000 | -0.220 | 21.562 | 0.105 | 4 | 0 | 0.0 |
| Ge1-O1-O1 | 1.000 | 1.384 | 2.034 | 0.000 | 1.000 | 0.000 | 9.258 | 2.119 | 4 | 0 | 0.0 |
| Ge1-O1-O2 | 1.000 | 0.000 | 0.000 | 94.550 | 1.000 | -0.058 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Ge1-Ge2 | 1.000 | 0.000 | 0.000 | 152.646 | 1.000 | -0.619 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 9.208 | 9.208 | 2.835 | 3.023 | 3.023 |
| or | 2.127 | 2.163 | 106.117 | 90.000 | 126.496 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 11.711 | 2.107 | 10.234 | 0.0 | 3.185 | |
| 8.879 | 1.612 | 10.945 | 0.0 | 3.096 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 82.293 | 106.117 | 2.107 | 2.107 | 0.0 | 3.185 | 0.0 | 3.185 | 0.0 | 4.082 | |
| 62.178 | 90.000 | 1.612 | 2.107 | 0.0 | 3.096 | 0.0 | 3.185 | 0.0 | 4.017 | |
| 96.214 | 126.496 | 1.612 | 2.107 | 0.0 | 3.096 | 0.0 | 3.185 | 0.0 | 4.426 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn1-O2-O2 | 1.000 | 2.107 | 1.512 | 82.293 | 1.000 | -0.278 | 11.711 | 0.519 | 4 | 0 | 0.0 |
| Sn1-O1-O1 | 1.000 | 1.612 | 1.921 | 0.000 | 1.000 | 0.000 | 8.879 | 1.623 | 4 | 0 | 0.0 |
| Sn1-O1-O2 | 1.000 | 0.000 | 0.000 | 62.178 | 1.000 | 0.000 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| O1-Sn1-Sn2 | 1.000 | 0.000 | 0.000 | 96.214 | 1.000 | -0.595 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 9.291 | 9.291 | 3.933 | 3.075 | 3.075 |
| or | 1.757 | 1.849 | 105.384 | 118.100 | 104.288 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 8.898 | 1.894 | 4.765 | 0.0 | 2.669 | |
| 5.791 | 1.220 | 5.844 | 0.0 | 2.600 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 134.527 | 105.384 | 1.894 | 1.894 | 0.0 | 2.669 | 0.0 | 2.669 | 0.0 | 3.559 | |
| 79.992 | 118.100 | 1.220 | 1.894 | 0.0 | 2.600 | 0.0 | 2.669 | 0.0 | 4.046 | |
| 66.283 | 104.288 | 1.220 | 1.894 | 0.0 | 2.600 | 0.0 | 2.669 | 0.0 | 3.921 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C1-S2-S2 | 1.000 | 1.894 | 1.410 | 134.527 | 1.000 | -0.265 | 8.898 | 0.371 | 4 | 0 | 0.0 |
| C1-S1-S1 | 1.000 | 1.220 | 2.131 | 0.000 | 1.000 | 0.000 | 5.791 | 2.637 | 4 | 0 | 0.0 |
| C1-S1-S2 | 1.000 | 0.000 | 0.000 | 79.992 | 1.000 | -0.471 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-C1-C2 | 1.000 | 0.000 | 0.000 | 66.283 | 1.000 | -0.247 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.135 | 7.135 | 2.512 | 2.922 | 2.922 |
| or | 2.300 | 2.344 | 93.554 | 96.500 | 111.710 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 3.878 | 0.797 | 13.992 | 0.0 | 2.977 | |
| 6.051 | 1.301 | 15.094 | 0.0 | 3.217 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 13.284 | 93.554 | 0.797 | 0.797 | 0.0 | 2.977 | 0.0 | 2.977 | 0.0 | 4.063 | |
| 21.310 | 96.500 | 1.301 | 0.797 | 0.0 | 3.217 | 0.0 | 2.977 | 0.0 | 4.232 | |
| 24.372 | 111.710 | 1.301 | 0.797 | 0.0 | 3.217 | 0.0 | 2.977 | 0.0 | 4.423 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si1-S2-S2 | 1.000 | 0.797 | 3.735 | 13.284 | 1.000 | -0.062 | 3.878 | 34.661 | 4 | 0 | 0.0 |
| Si1-S1-S1 | 1.000 | 1.301 | 2.474 | 0.000 | 1.000 | 0.000 | 6.051 | 5.276 | 4 | 0 | 0.0 |
| Si1-S1-S2 | 1.000 | 0.000 | 0.000 | 21.310 | 1.000 | -0.113 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Si1-Si2 | 1.000 | 0.000 | 0.000 | 24.372 | 1.000 | -0.370 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 6.364 | 6.364 | 2.153 | 3.896 | 3.896 |
| or | 2.462 | 2.423 | 95.402 | 94.400 | 104.837 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 2.096 | 0.351 | 18.371 | 0.0 | 2.926 | |
| 6.694 | 1.571 | 17.234 | 0.0 | 3.398 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 4.905 | 95.402 | 0.350 | 0.350 | 0.0 | 2.926 | 0.0 | 2.926 | 0.0 | 4.067 | |
| 20.842 | 94.400 | 1.571 | 0.350 | 0.0 | 3.398 | 0.0 | 2.926 | 0.0 | 4.292 | |
| 22.173 | 104.837 | 1.571 | 0.350 | 0.0 | 3.398 | 0.0 | 2.296 | 0.0 | 4.438 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge1-S4-S4 | 1.000 | 0.351 | 8.332 | 4.905 | 1.000 | -0.094 | 2.096 | 1227.130 | 4 | 0 | 0.0 |
| Ge1-S1-S1 | 1.000 | 1.571 | 2.163 | 0.000 | 1.000 | 0.000 | 6.694 | 2.830 | 4 | 0 | 0.0 |
| Ge1-S1-S4 | 1.000 | 0.000 | 0.000 | 20.842 | 1.000 | -0.077 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Ge1-Ge2 | 1.000 | 0.000 | 0.000 | 22.173 | 1.000 | -0.256 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 4.163 | 4.163 | 1.776 | 5.841 | 5.841 |
| or | 2.728 | 2.595 | 95.762 | 89.000 | 101.887 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 0.782 | 0.106 | 27.692 | 0.0 | 2.997 | |
| 5.636 | 1.887 | 22.674 | 0.0 | 3.702 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 1.968 | 95.762 | 0.106 | 0.106 | 0.0 | 2.997 | 0.0 | 2.997 | 0.0 | 4.197 | |
| 23.839 | 89.000 | 1.887 | 0.106 | 0.0 | 3.702 | 0.0 | 2.997 | 0.0 | 4.366 | |
| 24.888 | 101.887 | 1.887 | 0.106 | 0.0 | 3.702 | 0.0 | 2.997 | 0.0 | 4.566 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn1-S4-S4 | 1.000 | 0.106 | 28.347 | 1.971 | 1.000 | -0.100 | 0.783 | 221784.222 | 4 | 0 | 0.0 |
| Sn1-S1-S1 | 1.000 | 1.887 | 1.961 | 0.000 | 1.000 | 0.000 | 5.636 | 1.787 | 4 | 0 | 0.0 |
| Sn1-S1-S4 | 1.000 | 0.000 | 0.000 | 23.839 | 1.000 | 0.017 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| S1-Sn1-Sn2 | 1.000 | 0.000 | 0.000 | 24.888 | 1.000 | -0.206 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 10.120 | 10.120 | 4.505 | 3.910 | 3.910 |
| or | 1.961 | 2.014 | 101.354 | 113.000 | 100.563 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 6.141 | 1.114 | 7.394 | 0.0 | 2.700 | |
| 7.411 | 1.316 | 8.226 | 0.0 | 2.828 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 47.768 | 101.354 | 1.114 | 1.114 | 0.0 | 2.700 | 0.0 | 2.700 | 0.0 | 3.667 | |
| 52.464 | 113.000 | 1.316 | 1.114 | 0.0 | 2.828 | 0.0 | 2.700 | 0.0 | 4.157 | |
| 46.000 | 100.563 | 1.316 | 1.114 | 0.0 | 2.828 | 0.0 | 2.700 | 0.0 | 4.032 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C1-Se4-Se4 | 1.000 | 1.114 | 2.424 | 47.768 | 1.000 | -0.197 | 6.141 | 4.802 | 4 | 0 | 0.0 |
| C1-Se1-Se1 | 1.000 | 1.316 | 2.149 | 0.000 | 1.000 | 0.000 | 7.411 | 2.743 | 4 | 0 | 0.0 |
| C1-Se1-Se4 | 1.000 | 0.000 | 0.000 | 52.464 | 1.000 | -0.391 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-C1-C2 | 1.000 | 0.000 | 0.000 | 46.000 | 1.000 | -0.183 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.192 | 7.192 | 3.222 | 5.890 | 5.890 |
| or | 2.524 | 2.448 | 95.513 | 98.200 | 97.686 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 1.883 | 0.230 | 20.292 | 0.0 | 2.905 | |
| 8.098 | 1.665 | 17.956 | 0.0 | 3.457 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 5.440 | 95.513 | 0.230 | 0.230 | 0.0 | 2.905 | 0.0 | 2.905 | 0.0 | 4.069 | |
| 28.616 | 98.200 | 1.665 | 0.230 | 0.0 | 3.457 | 0.0 | 2.905 | 0.0 | 4.379 | |
| 28.545 | 97.686 | 1.665 | 0.230 | 0.0 | 3.457 | 0.0 | 2.905 | 0.0 | 4.369 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si1-Se4-Se4 | 1.000 | 0.230 | 12.628 | 5.440 | 1.000 | -0.096 | 1.883 | 7245.111 | 4 | 0 | 0.0 |
| Si1-Se1-Se1 | 1.000 | 1.665 | 2.076 | 0.000 | 1.000 | 0.000 | 8.098 | 2.335 | 4 | 0 | 0.0 |
| Si1-Se1-Se4 | 1.000 | 0.000 | 0.000 | 28.616 | 1.000 | -0.143 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Si1-Si2 | 1.000 | 0.000 | 0.000 | 28.545 | 1.000 | -0.134 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 5.063 | 5.063 | 2.249 | 5.927 | 5.927 |
| or | 2.661 | 2.544 | 96.322 | 97.000 | 93.964 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 0.962 | 0.115 | 25.070 | 0.0 | 2.938 | |
| 6.572 | 1.846 | 20.943 | 0.0 | 3.628 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 2.614 | 96.322 | 0.115 | 0.115 | 0.0 | 2.938 | 0.0 | 2.938 | 0.0 | 4.133 | |
| 25.087 | 97.400 | 1.846 | 0.115 | 0.0 | 3.628 | 0.0 | 2.938 | 0.0 | 4.455 | |
| 24.789 | 93.964 | 1.846 | 0.155 | 0.0 | 3.628 | 0.0 | 2.938 | 0.0 | 4.404 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge1-Se4-Se4 | 1.000 | 0.115 | 25.561 | 2.614 | 1.000 | -0.110 | 0.962 | 143723.555 | 4 | 0 | 0.0 |
| Ge1-Se1-Se1 | 1.000 | 1.846 | 1.965 | 0.000 | 1.000 | 0.000 | 6.572 | 1.804 | 4 | 0 | 0.0 |
| Ge1-Se1-Se4 | 1.000 | 0.000 | 0.000 | 25.087 | 1.000 | -0.129 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Ge1-Ge2 | 1.000 | 0.000 | 0.000 | 24.789 | 1.000 | -0.069 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 3.872 | 3.872 | 3.157 | 7.674 | 7.674 |
| or | 2.887 | 2.730 | 95.087 | 92.500 | 95.411 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 0.565 | 0.056 | 34.734 | 0.0 | 3.088 | |
| 5.811 | 1.989 | 27.773 | 0.0 | 3.895 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 2.777 | 95.087 | 0.056 | 0.056 | 0.0 | 3.088 | 0.0 | 3.088 | 0.0 | 4.357 | |
| 27.996 | 92.500 | 1.989 | 0.056 | 0.0 | 3.895 | 0.0 | 3.088 | 0.0 | 4.530 | |
| 28.193 | 95.411 | 1.989 | 0.056 | 0.0 | 3.895 | 0.0 | 3.088 | 0.0 | 4.576 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn1-Se4-Se4 | 1.000 | 0.056 | 55.166 | 2.777 | 1.000 | -0.089 | 0.565 | 3537820.961 | 4 | 0 | 0.0 |
| Sn1-Se1-Se1 | 1.000 | 1.989 | 1.959 | 0.000 | 1.000 | 0.000 | 5.811 | 1.776 | 4 | 0 | 0.0 |
| Sn1-Se1-Se4 | 1.000 | 0.000 | 0.000 | 27.996 | 1.000 | -0.044 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Se1-Sn1-Sn2 | 1.000 | 0.000 | 0.000 | 28.193 | 1.000 | -0.094 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 13.235 | 13.235 | 4.210 | 3.901 | 3.901 |
| or | 2.164 | 2.181 | 103.122 | 110.000 | 90.854 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 4.165 | 0.424 | 10.965 | 0.0 | 2.643 | |
| 12.519 | 1.569 | 11.313 | 0.0 | 3.106 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 13.040 | 103.122 | 0.424 | 0.424 | 0.0 | 2.643 | 0.0 | 2.643 | 0.0 | 3.639 | |
| 29.206 | 110.000 | 1.569 | 0.424 | 0.0 | 3.106 | 0.0 | 2.643 | 0.0 | 4.280 | |
| 25.795 | 90.854 | 1.569 | 0.424 | 0.0 | 3.106 | 0.0 | 2.643 | 0.0 | 4.043 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C1-Te4-Te4 | 1.000 | 0.424 | 6.232 | 13.040 | 1.000 | -0.227 | 4.165 | 338.925 | 4 | 0 | 0.0 |
| C1-Te1-Te1 | 1.000 | 1.569 | 1.979 | 0.000 | 1.000 | 0.000 | 12.519 | 1.866 | 4 | 0 | 0.0 |
| C1-Te1-Te4 | 1.000 | 0.000 | 0.000 | 29.206 | 1.000 | -0.342 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-C1-C2 | 1.000 | 0.000 | 0.000 | 25.795 | 1.000 | -0.015 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 9.479 | 2.892 | 3.145 | 10.111 | 10.111 |
| or | 2.641 | 2.772 | 102.142 | 100.200 | 92.760 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 2.394 | 0.194 | 24.324 | 0.0 | 2.999 | |
| 3.818 | 1.722 | 29.522 | 0.0 | 3.864 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 4.868 | 102.142 | 0.194 | 0.194 | 0.0 | 2.999 | 0.0 | 2.999 | 0.0 | 4.204 | |
| 43.419 | 100.200 | 1.722 | 0.194 | 0.0 | 3.864 | 0.0 | 2.999 | 0.0 | 4.577 | |
| 42.155 | 92.760 | 1.722 | 0.194 | 0.0 | 3.864 | 0.0 | 2.999 | 0.0 | 4.289 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si1-Te4-Te4 | 1.000 | 0.194 | 15.442 | 4.868 | 1.000 | -0.210 | 2.394 | 17093.960 | 4 | 0 | 0.0 |
| Si1-Te1-Te1 | 1.000 | 1.722 | 2.245 | 0.000 | 1.000 | 0.000 | 3.818 | 3.360 | 4 | 0 | 0.0 |
| Si1-Te1-Te4 | 1.000 | 0.000 | 0.000 | 43.419 | 1.000 | -0.177 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Si1-Si2 | 1.000 | 0.000 | 0.000 | 42.155 | 1.000 | -0.048 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.074 | 7.074 | 2.611 | 5.876 | 5.876 |
| or | 2.736 | 2.883 | 101.517 | 100.400 | 91.402 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 1.708 | 0.165 | 28.018 | 0.0 | 3.072 | |
| 9.854 | 1.745 | 34.542 | 0.0 | 4.005 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 3.626 | 101.517 | 0.165 | 0.165 | 0.0 | 3.072 | 0.0 | 3.072 | 0.0 | 4.307 | |
| 23.509 | 100.400 | 1.745 | 0.165 | 0.0 | 4.005 | 0.0 | 3.072 | 0.0 | 4.659 | |
| 22.756 | 91.402 | 1.745 | 0.165 | 0.0 | 4.005 | 0.0 | 3.072 | 0.0 | 4.434 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge1-Te4-Te4 | 1.000 | 0.165 | 18.665 | 3.626 | 1.000 | -0.200 | 1.708 | 38204.858 | 4 | 0 | 0.0 |
| Ge1-Te1-Te1 | 1.000 | 1.745 | 2.295 | 0.000 | 1.000 | 0.000 | 9.854 | 3.725 | 4 | 0 | 0.0 |
| Ge1-Te1-Te4 | 1.000 | 0.000 | 0.000 | 23.509 | 1.000 | -0.181 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Ge1-Ge2 | 1.000 | 0.000 | 0.000 | 22.756 | 1.000 | -0.024 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | |||
|---|---|---|---|---|---|
| expression | |||||
| parameter | 7.074 | 7.074 | 2.611 | 2.611 | 5.876 |
| or | 2.931 | 3.164 | 101.578 | 96.000 | 94.045 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 1.662 | 0.131 | 36.901 | 0.0 | 3.241 | |
| 11.054 | 1.777 | 50.109 | 0.0 | 4.349 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 3.170 | 101.578 | 0.131 | 0.131 | 0.0 | 3.241 | 0.0 | 3.241 | 0.0 | 4.562 | |
| 20.298 | 96.000 | 1.777 | 0.131 | 0.0 | 4.349 | 0.0 | 3.241 | 0.0 | 4.766 | |
| 20.176 | 94.045 | 1.777 | 0.131 | 0.0 | 4.349 | 0.0 | 3.241 | 0.0 | 4.595 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn1-Te4-Te4 | 1.000 | 0.131 | 24.712 | 3.170 | 1.000 | -0.201 | 1.662 | 124727.735 | 4 | 0 | 0.0 |
| Sn1-Te1-Te1 | 1.000 | 1.777 | 2.448 | 0.000 | 1.000 | 0.000 | 11.054 | 5.028 | 4 | 0 | 0.0 |
| Sn1-Te1-Te4 | 1.000 | 0.000 | 0.000 | 20.298 | 1.000 | -0.105 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| Te1-Sn1-Sn2 | 1.000 | 0.000 | 0.000 | 20.176 | 1.000 | -0.071 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 18.387 | 3.465 |
| or | 2.279 | 116.218 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-Si | 19.343 | 1.668 | 16.186 | 0.0 | 3.075 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-Si-Si | 142.310 | 116.218 | 1.668 | 1.668 | 0.0 | 3.075 | 0.0 | 3.075 | 3.075 | 4.181 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-Si-Si | 1.000 | 1.668 | 1.844 | 142.310 | 1.000 | -0.442 | 19.343 | 2.091 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 18.387 | 3.465 |
| or | 2.443 | 112.358 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ge-Ge | 19.570 | 1.607 | 21.372 | 0.0 | 3.252 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Ge-Ge | 107.735 | 112.358 | 1.607 | 1.607 | 0.0 | 3.252 | 0.0 | 3.252 | 3.252 | 4.4 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Ge-Ge | 1.000 | 1.607 | 2.024 | 107.735 | 1.000 | -0.380 | 19.570 | 3.205 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 10.489 | 1.372 |
| or | 2.836 | 111.224 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-Sn | 19.542 | 2.227 | 42.047 | 0.0 | 3.758 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Sn-Sn | 98.863 | 111.224 | 2.227 | 2.227 | 0.0 | 3.758 | 0.0 | 3.758 | 3.758 | 5.076 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Sn-Sn | 1.000 | 2.227 | 1.687 | 98.863 | 1.000 | -0.362 | 19.542 | 1.709 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 2.128 | 1.175 |
| or | 2.890 | 94.372 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In-In | 1.537 | 0.946 | 41.855 | 0.0 | 3.565 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In-In-In | 9.745 | 94.372 | 0.946 | 0.946 | 0.0 | 3.565 | 0.0 | 4.565 | 3.565 | 4.686 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In-In-In | 1.000 | 0.946 | 3.768 | 9.745 | 1.000 | -0.076 | 1.537 | 52.262 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 15.372 | 5.138 |
| or | 2.270 | 94.209 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| P-P | 5.706 | 0.491 | 13.276 | 0.0 | 2.798 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| P-P-P | 16.605 | 94.209 | 0.491 | 0.491 | 0.0 | 2.798 | 0.0 | 2.798 | 2.798 | 3.677 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| P-P-P | 1.000 | 0.491 | 5.699 | 16.605 | 1.000 | -0.073 | 5.706 | 228.424 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 15.372 | 5.138 |
| or | 2.510 | 91.964 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| As-As | 6.418 | 0.482 | 19.846 | 0.0 | 3.060 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| As-As-As | 14.845 | 91.964 | 0.482 | 0.482 | 0.0 | 3.060 | 0.0 | 3.060 | 3.060 | 4.004 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| As-As-As | 1.000 | 0.482 | 6.349 | 14.845 | 1.000 | -0.034 | 6.418 | 367.693 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 15.372 | 5.138 |
| or | 2.890 | 90.927 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sb-Sb | 8.173 | 0.523 | 34.879 | 0.0 | 3.505 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sb-Sb-Sb | 14.100 | 90.927 | 0.523 | 0.523 | 0.0 | 3.505 | 0.0 | 3.503 | 3.505 | 4.577 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sb-Sb-Sb | 1.000 | 0.523 | 6.702 | 14.100 | 1.000 | -0.016 | 8.173 | 466.184 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 11.529 | 3.853 |
| or | 3.045 | 90.901 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Bi-Bi | 6.805 | 0.552 | 42.985 | 0.0 | 3.693 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Bi-Bi-Bi | 10.574 | 90.901 | 0.552 | 0.552 | 0.0 | 3.693 | 0.0 | 3.693 | 3.693 | 4.821 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Bi-Bi-Bi | 1.000 | 0.552 | 6.690 | 10.574 | 1.000 | -0.016 | 6.805 | 462.978 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 16.063 | 5.221 |
| or | 1.636 | 97.181 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| C-O | 7.656 | 1.054 | 3.582 | 0.0 | 2.293 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| C-O-O | 65.778 | 97.181 | 1.054 | 1.054 | 0.0 | 2.293 | 0.0 | 2.293 | 0.0 | 3.352 |
| O-C-C | 65.778 | 97.181 | 1.054 | 1.054 | 0.0 | 2.293 | 0.0 | 2.293 | 0.0 | 3.352 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C-O-O | 1.000 | 1.054 | 2.175 | 65.778 | 1.000 | -0.125 | 7.812 | 2.900 | 4 | 0 | 0.0 |
| O-C-C | 1.000 | 1.054 | 2.175 | 65.778 | 1.000 | -0.125 | 7.812 | 2.900 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 9.390 | 4.722 |
| or | 1.880 | 97.921 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| C-S | 6.014 | 1.233 | 6.246 | 0.0 | 2.641 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| C-S-S | 61.413 | 97.921 | 1.233 | 1.233 | 0.0 | 2.641 | 0.0 | 2.641 | 0.0 | 3.874 |
| S-C-C | 61.413 | 97.921 | 1.233 | 1.233 | 0.0 | 2.641 | 0.0 | 2.641 | 0.0 | 3.874 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C-S-S | 1.000 | 1.233 | 2.142 | 61.413 | 1.000 | -0.138 | 6.014 | 2.703 | 4 | 0 | 0.0 |
| S-C-C | 1.000 | 1.233 | 2.142 | 61.413 | 1.000 | -0.138 | 6.014 | 2.703 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 10.425 | 5.031 |
| or | 2.055 | 96.362 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| C-Se | 7.691 | 1.298 | 8.917 | 0.0 | 2.872 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| C-Se-Se | 61.215 | 96.362 | 1.298 | 1.298 | 0.0 | 2.872 | 0.0 | 2.872 | 0.0 | 4.184 |
| Se-C-C | 61.215 | 96.362 | 1.298 | 1.298 | 0.0 | 2.872 | 0.0 | 2.872 | 0.0 | 4.184 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C-Se-Se | 1.000 | 1.298 | 2.212 | 61.215 | 1.000 | -0.111 | 7.691 | 3.137 | 4 | 0 | 0.0 |
| Se-C-C | 1.000 | 1.298 | 2.212 | 61.215 | 1.000 | -0.111 | 7.691 | 3.137 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 9.367 | 4.311 |
| or | 2.231 | 97.239 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| C-Te | 8.314 | 1.440 | 12.387 | 0.0 | 3.127 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| C-Te-Te | 54.451 | 97.239 | 1.440 | 1.440 | 0.0 | 3.127 | 0.0 | 3.127 | 0.0 | 4.573 |
| Te-C-C | 54.451 | 97.239 | 1.440 | 1.440 | 0.0 | 3.127 | 0.0 | 3.127 | 0.0 | 4.573 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| C-Te-Te | 1.000 | 1.440 | 2.172 | 54.451 | 1.000 | -0.126 | 8.314 | 2.883 | 4 | 0 | 0.0 |
| Te-C-C | 1.000 | 1.440 | 2.172 | 54.451 | 1.000 | -0.126 | 8.314 | 2.883 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 9.315 | 3.300 |
| or | 1.884 | 96.676 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-O | 5.819 | 1.200 | 6.299 | 0.0 | 2.636 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-O-O | 40.695 | 96.676 | 1.200 | 1.200 | 0.0 | 2.636 | 0.0 | 2.636 | 0.0 | 3.845 |
| O-Si-Si | 40.695 | 96.676 | 1.200 | 1.200 | 0.0 | 2.636 | 0.0 | 2.636 | 0.0 | 3.845 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-O-O | 1.000 | 1.200 | 2.197 | 40.695 | 1.000 | -0.116 | 5.819 | 3.043 | 4 | 0 | 0.0 |
| O-Si-Si | 1.000 | 1.200 | 2.197 | 40.695 | 1.000 | -0.116 | 5.819 | 3.043 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.441 | 4.802 |
| or | 2.321 | 90.581 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-S | 6.897 | 1.264 | 14.510 | 0.0 | 3.177 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-S-S | 45.954 | 90.581 | 1.264 | 1.264 | 0.0 | 3.177 | 0.0 | 3.177 | 0.0 | 4.506 |
| S-Si-Si | 45.954 | 90.581 | 1.264 | 1.264 | 0.0 | 3.177 | 0.0 | 3.177 | 0.0 | 4.506 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-S-S | 1.000 | 1.264 | 2.514 | 45.954 | 1.000 | -0.010 | 6.897 | 5.687 | 4 | 0 | 0.0 |
| S-Si-Si | 1.000 | 1.264 | 2.514 | 45.954 | 1.000 | -0.010 | 6.897 | 5.687 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.441 | 4.802 |
| or | 2.477 | 90.590 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-Se | 7.857 | 1.349 | 18.822 | 0.0 | 3.391 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-Se-Se | 45.968 | 90.590 | 1.349 | 1.349 | 0.0 | 3.391 | 0.0 | 3.391 | 0.0 | 4.810 |
| Se-Si-Si | 45.968 | 90.590 | 1.349 | 1.349 | 0.0 | 3.391 | 0.0 | 3.391 | 0.0 | 4.810 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-Se-Se | 1.000 | 1.349 | 2.514 | 45.968 | 1.000 | -0.010 | 7.857 | 5.6683 | 4 | 0 | 0.0 |
| Se-Si-Si | 1.000 | 1.349 | 2.514 | 45.968 | 1.000 | -0.010 | 7.857 | 5.6683 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.418 | 4.349 |
| or | 2.690 | 90.779 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-Te | 9.285 | 1.473 | 26.181 | 0.0 | 3.685 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-Te-Te | 41.952 | 90.779 | 1.473 | 1.473 | 0.0 | 3.685 | 0.0 | 3.685 | 0.0 | 5.232 |
| Te-Si-Si | 41.952 | 90.779 | 1.473 | 1.473 | 0.0 | 3.685 | 0.0 | 3.685 | 0.0 | 5.232 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-Te-Te | 1.000 | 0.725 | 4.497 | 27.653 | 1.000 | -0.014 | 4.428 | 113.714 | 4 | 0 | 0.0 |
| Te-Si-Si | 1.000 | 0.725 | 4.497 | 27.653 | 1.000 | -0.014 | 4.428 | 113.714 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 9.315 | 3.300 |
| or | 2.032 | 100.475 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ge-O | 7.390 | 1.413 | 8.524 | 0.0 | 2.879 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ge-O-O | 47.962 | 100.475 | 1.413 | 1.413 | 0.0 | 2.879 | 0.0 | 2.879 | 0.0 | 4.267 |
| O-Ge-Ge | 47.962 | 100.475 | 1.413 | 1.413 | 0.0 | 2.879 | 0.0 | 2.879 | 0.0 | 4.267 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge-O-O | 1.000 | 1.413 | 2.037 | 47.962 | 1.000 | -0.182 | 7.390 | 2.136 | 4 | 0 | 0.0 |
| O-Ge-Ge | 1.000 | 1.413 | 2.037 | 47.962 | 1.000 | -0.182 | 7.390 | 2.136 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.322 | 3.516 |
| or | 2.428 | 91.725 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ge-S | 7.657 | 1.363 | 17.377 | 0.0 | 3.338 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ge-S-S | 35.249 | 91.725 | 1.363 | 1.363 | 0.0 | 3.338 | 0.0 | 3.338 | 0.0 | 4.761 |
| S-Ge-Ge | 35.249 | 91.725 | 1.363 | 1.363 | 0.0 | 3.338 | 0.0 | 3.338 | 0.0 | 4.761 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge-S-S | 1.000 | 1.363 | 2.448 | 35.249 | 1.000 | -0.030 | 7.657 | 5.030 | 4 | 0 | 0.0 |
| S-Ge-Ge | 1.000 | 1.363 | 2.448 | 35.249 | 1.000 | -0.030 | 7.657 | 5.030 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.322 | 3.516 |
| or | 2.568 | 91.406 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ge-Se | 8.498 | 1.430 | 21.745 | 0.0 | 3.526 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Se-Se | 34.791 | 91.406 | 1.430 | 1.430 | 0.0 | 3.526 | 0.0 | 3.526 | 0.0 | 5.021 |
| Se-Ge-Ge | 34.791 | 91.406 | 1.430 | 1.430 | 0.0 | 3.526 | 0.0 | 3.526 | 0.0 | 5.021 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Se-Se | 1.000 | 1.430 | 2.466 | 34.791 | 1.000 | -0.025 | 8.498 | 5.205 | 4 | 0 | 0.0 |
| Se-Ge-Ge | 1.000 | 1.430 | 2.466 | 34.791 | 1.000 | -0.025 | 8.498 | 5.205 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.322 | 3.516 |
| or | 2.768 | 90.718 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ge-Te | 9.704 | 1.513 | 29.352 | 0.0 | 3.791 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Te-Te | 33.832 | 90.718 | 1.513 | 1.513 | 0.0 | 3.791 | 0.0 | 3.791 | 0.0 | 5.381 |
| Te-Ge-Ge | 33.832 | 90.718 | 1.513 | 1.513 | 0.0 | 3.791 | 0.0 | 3.791 | 0.0 | 5.381 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ge-Te-Te | 1.000 | 1.513 | 2.506 | 33.832 | 1.000 | -0.013 | 9.704 | 5.605 | 4 | 0 | 0.0 |
| Te-Ge-Ge | 1.000 | 1.513 | 2.506 | 33.832 | 1.000 | -0.013 | 9.704 | 5.605 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 9.315 | 3.300 |
| or | 2.204 | 102.677 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-O | 9.133 | 1.609 | 11.798 | 0.0 | 3.146 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-O-O | 52.875 | 102.677 | 1.609 | 1.609 | 0.0 | 3.146 | 0.0 | 3.146 | 0.0 | 4.702 |
| O-Sn-Sn | 52.875 | 102.677 | 1.609 | 1.609 | 0.0 | 3.146 | 0.0 | 3.146 | 0.0 | 4.702 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-O-O | 1.000 | 1.609 | 1.955 | 52.875 | 1.000 | -0.219 | 9.133 | 1.760 | 4 | 0 | 0.0 |
| O-Sn-Sn | 1.000 | 1.609 | 1.955 | 52.875 | 1.000 | -0.219 | 9.133 | 1.760 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 6.909 | 2.710 |
| or | 2.616 | 91.793 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-S | 7.392 | 1.472 | 23.416 | 0.0 | 3.597 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-S-S | 27.243 | 91.793 | 1.472 | 1.472 | 0.0 | 3.597 | 0.0 | 3.597 | 0.0 | 5.132 |
| S-Sn-Sn | 27.243 | 91.793 | 1.472 | 1.472 | 0.0 | 3.597 | 0.0 | 3.597 | 0.0 | 5.132 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-S-S | 1.000 | 1.472 | 2.444 | 27.243 | 1.000 | -0.031 | 7.392 | 4.994 | 4 | 0 | 0.0 |
| S-Sn-Sn | 1.000 | 1.472 | 2.444 | 27.243 | 1.000 | -0.031 | 7.392 | 4.994 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 6.909 | 2.710 |
| or | 2.747 | 90.923 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-Se | 7.976 | 1.510 | 28.471 | 0.0 | 3.765 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Se-Se | 26.294 | 90.923 | 1.510 | 1.510 | 0.0 | 3.765 | 0.0 | 3.765 | 0.0 | 5.349 |
| Se-Sn-Sn | 26.294 | 90.923 | 1.510 | 1.510 | 0.0 | 3.765 | 0.0 | 3.765 | 0.0 | 5.349 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Se-Se | 1.000 | 1.510 | 2.494 | 26.294 | 1.000 | -0.016 | 7.976 | 5.482 | 4 | 0 | 0.0 |
| Se-Sn-Sn | 1.000 | 1.510 | 2.494 | 26.294 | 1.000 | -0.016 | 7.976 | 5.482 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 6.909 | 2.710 |
| or | 2.947 | 89.542 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-Te | 8.864 | 1.559 | 37.713 | 0.0 | 4.019 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Te-Te | 24.867 | 89.542 | 1.559 | 1.559 | 0.0 | 4.019 | 0.0 | 4.019 | 0.0 | 5.670 |
| Te-Sn-Sn | 24.867 | 89.542 | 1.559 | 1.559 | 0.0 | 4.019 | 0.0 | 4.019 | 0.0 | 5.670 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Te-Te | 1.000 | 1.559 | 2.577 | 24.867 | 1.000 | 0.008 | 8.864 | 6.378 | 4 | 0 | 0.0 |
| Te-Sn-Sn | 1.000 | 1.559 | 2.577 | 24.867 | 1.000 | 0.008 | 8.864 | 6.378 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.390 | 3.112 |
| or | 2.570 | 112.350 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-Ge | 13.674 | 2.267 | 21.812 | 0.0 | 3.777 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Ge-Ge | 77.881 | 112.350 | 2.267 | 2.267 | 0.0 | 3.777 | 0.0 | 3.777 | 0.0 | 5.833 |
| Ge-Sn-Sn | 77.881 | 112.350 | 2.267 | 2.267 | 0.0 | 3.777 | 0.0 | 3.777 | 0.0 | 5.833 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Ge-Ge | 1.000 | 2.267 | 1.666 | 77.881 | 1.000 | -0.380 | 13.674 | 0.826 | 4 | 0 | 0.0 |
| Ge-Sn-Sn | 1.000 | 2.267 | 1.666 | 77.881 | 1.000 | -0.380 | 13.674 | 0.826 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 16.390 | 3.112 |
| or | 2.310 | 114.702 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Si-Ge | 22.576 | 2.122 | 14.237 | 0.0 | 3.417 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Si-Ge-Ge | 87.197 | 114.702 | 2.122 | 2.122 | 0.0 | 3.417 | 0.0 | 3.417 | 0.0 | 5.314 |
| Ge-Si-Si | 87.197 | 114.702 | 2.122 | 2.122 | 0.0 | 3.417 | 0.0 | 3.417 | 0.0 | 5.314 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Si-Ge-Ge | 1.000 | 2.122 | 1.610 | 87.197 | 1.000 | -0.418 | 22.576 | 0.702 | 4 | 0 | 0.0 |
| Ge-Si-Si | 1.000 | 2.122 | 1.610 | 87.197 | 1.000 | -0.418 | 22.576 | 0.702 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 10.315 | 2.880 |
| or | 2.520 | 113.298 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Sn-Si | 16.463 | 2.260 | 20.164 | 0.0 | 3.713 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Si-Si | 75.415 | 113.298 | 2.260 | 2.260 | 0.0 | 3.713 | 0.0 | 3.713 | 0.0 | 5.751 |
| Si-Sn-Sn | 75.415 | 113.298 | 2.260 | 2.260 | 0.0 | 3.713 | 0.0 | 3.713 | 0.0 | 5.751 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Sn-Si-Si | 1.000 | 2.260 | 1.643 | 75.415 | 1.000 | -0.396 | 16.463 | 0.773 | 4 | 0 | 0.0 |
| Si-Sn-Sn | 1.000 | 2.260 | 1.643 | 75.415 | 1.000 | -0.396 | 16.463 | 0.773 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 12.903 | 2.384 |
| or | 2.460 | 115.895 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In-P | 20.610 | 2.306 | 18.311 | 0.0 | 3.651 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In-P-P | 70.782 | 115.895 | 2.306 | 2.306 | 0.0 | 3.651 | 0.0 | 3.651 | 0.0 | 5.696 |
| P-In-In | 70.782 | 115.895 | 2.306 | 2.306 | 0.0 | 3.651 | 0.0 | 3.651 | 0.0 | 5.696 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In-P-P | 1.000 | 2.306 | 1.583 | 70.782 | 1.000 | -0.437 | 20.610 | 0.648 | 4 | 0 | 0.0 |
| P-In-In | 1.000 | 2.306 | 1.583 | 70.782 | 1.000 | -0.437 | 20.610 | 0.648 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 10.903 | 2.384 |
| or | 2.550 | 114.115 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In-As | 18.099 | 2.320 | 21.141 | 0.0 | 3.766 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In-As-As | 64.931 | 114.115 | 2.320 | 2.320 | 0.0 | 3.766 | 0.0 | 3.766 | 0.0 | 5.847 |
| As-In-In | 64.931 | 114.115 | 2.320 | 2.320 | 0.0 | 3.766 | 0.0 | 3.766 | 0.0 | 5.847 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In-As-As | 1.000 | 2.320 | 1.624 | 64.931 | 1.000 | -0.409 | 18.099 | 0.730 | 4 | 0 | 0.0 |
| As-In-In | 1.000 | 2.320 | 1.624 | 64.931 | 1.000 | -0.409 | 18.099 | 0.730 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 8.903 | 2.384 |
| or | 2.740 | 113.012 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In-Sb | 16.706 | 2.445 | 28.182 | 0.0 | 4.034 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In-Sb-Sb | 61.578 | 113.012 | 2.445 | 2.445 | 0.0 | 4.034 | 0.0 | 4.034 | 0.0 | 6.243 |
| Sb-In-In | 61.578 | 113.012 | 2.445 | 2.445 | 0.0 | 4.034 | 0.0 | 4.034 | 0.0 | 6.243 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In-Sb-Sb | 1.000 | 2.445 | 1.650 | 61.578 | 1.000 | -0.391 | 16.706 | 0.788 | 4 | 0 | 0.0 |
| Sb-In-In | 1.000 | 2.445 | 1.650 | 61.578 | 1.000 | -0.391 | 16.706 | 0.788 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 12.903 | 3.284 |
| or | 2.360 | 114.513 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga-As | 18.485 | 2.161 | 15.510 | 0.0 | 3.489 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga-As-As | 91.177 | 114.513 | 2.161 | 2.161 | 0.0 | 3.489 | 0.0 | 3.489 | 0.0 | 5.423 |
| As-Ga-Ga | 91.177 | 114.513 | 2.161 | 2.161 | 0.0 | 3.489 | 0.0 | 3.489 | 0.0 | 5.423 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga-As-As | 1.000 | 2.161 | 1.614 | 91.177 | 1.000 | -0.415 | 18.485 | 0.711 | 4 | 0 | 0.0 |
| As-Ga-Ga | 1.000 | 2.161 | 1.614 | 91.177 | 1.000 | -0.415 | 18.485 | 0.711 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 16.050 | 3.022 |
| or | 2.250 | 117.152 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga-P | 21.948 | 2.152 | 12.814 | 0.0 | 3.350 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga-P-P | 95.438 | 117.152 | 2.152 | 2.152 | 0.0 | 3.350 | 0.0 | 3.350 | 0.0 | 5.246 |
| P-Ga-Ga | 95.438 | 117.152 | 2.152 | 2.152 | 0.0 | 3.350 | 0.0 | 3.350 | 0.0 | 5.246 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga-P-P | 1.000 | 2.152 | 1.557 | 95.438 | 1.000 | -0.456 | 21.948 | 0.597 | 4 | 0 | 0.0 |
| P-Ga-Ga | 1.000 | 2.152 | 1.557 | 95.438 | 1.000 | -0.456 | 21.948 | 0.597 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending |
|---|---|---|
| expression | ||
| parameter | 12.050 | 3.022 |
| or | 2.570 | 114.791 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Al-Sb | 20.580 | 2.365 | 21.812 | 0.0 | 3.803 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Al-Sb-Sb | 85.046 | 114.791 | 2.365 | 2.365 | 0.0 | 3.803 | 0.0 | 3.803 | 0.0 | 5.915 |
| Sb-Al-Al | 85.046 | 114.791 | 2.365 | 2.365 | 0.0 | 3.803 | 0.0 | 3.803 | 0.0 | 5.915 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Al-Sb-Sb | 1.000 | 2.365 | 1.608 | 85.046 | 1.000 | -0.419 | 20.580 | 0.697 | 4 | 0 | 0.0 |
| Sb-Al-Al | 1.000 | 2.365 | 1.608 | 85.046 | 1.000 | -0.419 | 20.580 | 0.697 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 23.030 | 15.512 | 5.577 | 6.209 |
| or | 1.520 | 1.770 | 106.764 | 112.059 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| B1-O1 | 11.725 | 1.207 | 2.669 | 0.0 | 2.197 |
| B1-B2 | 6.749 | 0.875 | 4.908 | 0.0 | 2.392 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| B1-O1-O1 | 107.486 | 106.764 | 1.207 | 1.207 | 0.0 | 2.197 | 0.0 | 2.197 | 0.0 | 3.333 |
| B1-B2-O1 | 87.662 | 112.059 | 0.875 | 1.207 | 0.0 | 2.392 | 0.0 | 2.197 | 0.0 | 3.198 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| B1-O1-O1 | 1.000 | 1.207 | 1.820 | 107.486 | 1.000 | -0.288 | 11.725 | 1.256 | 4 | 0 | 0.0 |
| B1-B2-B2 | 1.000 | 0.875 | 2.734 | 0.000 | 1.000 | 0.000 | 6.749 | 8.377 | 4 | 0 | 0.0 |
| B1-B2-O1 | 1.000 | 0.000 | 0.000 | 87.662 | 1.000 | -0.376 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 18.189 | 6.410 | 3.182 | 1.318 |
| or | 1.830 | 2.620 | 107.947 | 110.956 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Al1-O1 | 13.758 | 1.488 | 5.608 | 0.0 | 2.655 |
| Al1-Al2 | 3.609 | 0.678 | 23.560 | 0.0 | 3.287 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Al1-O1-O1 | 64.759 | 107.947 | 1.488 | 1.488 | 0.0 | 2.655 | 0.0 | 2.655 | 0.0 | 4.043 |
| Al1-O1-Al2 | 12.688 | 110.956 | 1.488 | 0.678 | 0.0 | 2.655 | 0.0 | 3.287 | 0.0 | 4.213 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Al1-O1-O1 | 1.000 | 1.488 | 1.785 | 64.759 | 1.000 | -0.308 | 13.758 | 1.145 | 4 | 0 | 0.0 |
| Al1-Al2-Al2 | 1.000 | 0.678 | 4.846 | 0.000 | 1.000 | 0.000 | 3.609 | 111.363 | 4 | 0 | 0.0 |
| Al1-Al2-O1 | 1.000 | 0.000 | 0.000 | 12.688 | 1.000 | -0.358 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 18.189 | 6.410 | 3.182 | 1.628 |
| or | 1.940 | 2.510 | 107.051 | 111.794 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga1-O1 | 15.178 | 1.550 | 7.082 | 0.0 | 2.807 |
| Ga1-Ga2 | 4.225 | 0.890 | 19.846 | 0.0 | 3.257 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-O1-O1 | 62.149 | 107.051 | 1.550 | 1.550 | 0.0 | 2.807 | 0.0 | 2.807 | 0.0 | 4.262 |
| Ga1-O1-Ga2 | 18.443 | 111.794 | 1.550 | 0.890 | 0.0 | 2.807 | 0.0 | 3.257 | 0.0 | 4.269 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-O1-O1 | 1.000 | 1.550 | 1.811 | 62.149 | 1.000 | -0.293 | 15.178 | 1.227 | 4 | 0 | 0.0 |
| Ga1-Ga2-Ga2 | 1.000 | 0.890 | 3.661 | 0.000 | 1.000 | 0.000 | 4.225 | 31.685 | 4 | 0 | 0.0 |
| Ga1-Ga2-O1 | 1.000 | 0.000 | 0.000 | 18.443 | 1.000 | -0.371 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 16.916 | 4.250 | 2.171 | 1.138 |
| or | 2.160 | 2.860 | 107.328 | 111.538 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In1-O1 | 17.600 | 1.735 | 10.884 | 0.0 | 3.128 |
| In1-In2 | 3.440 | 0.945 | 33.453 | 0.0 | 3.682 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In1-O1-O1 | 42.946 | 107.328 | 1.735 | 1.735 | 0.0 | 3.128 | 0.0 | 3.128 | 0.0 | 4.754 |
| In1-O1-In2 | 12.470 | 111.538 | 1.735 | 0.945 | 0.0 | 3.128 | 0.0 | 3.682 | 0.0 | 4.800 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In1-O1-O1 | 1.000 | 1.735 | 1.803 | 42.946 | 1.000 | -0.298 | 17.600 | 1.201 | 4 | 0 | 0.0 |
| In1-In2-In2 | 1.000 | 0.945 | 3.895 | 0.000 | 1.000 | 0.000 | 3.440 | 41.864 | 4 | 0 | 0.0 |
| In1-In2-O1 | 1.000 | 0.000 | 0.000 | 12.470 | 1.000 | -0.367 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 17.138 | 16.385 | 5.144 | 3.861 |
| or | 1.940 | 1.720 | 102.691 | 115.613 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| B1-S1 | 13.021 | 1.417 | 7.082 | 0.0 | 2.769 |
| B1-B2 | 14.613 | 1.809 | 4.376 | 0.0 | 2.602 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| B1-S1-S1 | 82.459 | 102.691 | 1.417 | 1.417 | 0.0 | 2.769 | 0.0 | 2.769 | 0.0 | 4.139 |
| B1-B2-S1 | 102.002 | 115.613 | 1.809 | 1.417 | 0.0 | 2.602 | 0.0 | 2.769 | 0.0 | 3.717 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| B1-S1-S1 | 1.000 | 1.417 | 1.955 | 82.459 | 1.000 | -0.220 | 13.021 | 1.758 | 4 | 0 | 0.0 |
| B1-B2-B2 | 1.000 | 1.809 | 1.438 | 0.000 | 1.000 | 0.000 | 14.613 | 0.408 | 4 | 0 | 0.0 |
| B1-B2-S1 | 1.000 | 0.000 | 0.000 | 102.002 | 1.000 | -0.432 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 11.065 | 4.912 | 3.210 | 1.900 |
| or | 2.320 | 2.590 | 100.600 | 117.324 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Al1-S1 | 11.476 | 1.618 | 14.485 | 0.0 | 3.289 |
| Al1-Al2 | 4.575 | 1.280 | 22.499 | 0.0 | 3.500 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Al1-S1-S1 | 46.910 | 100.600 | 1.618 | 1.618 | 0.0 | 3.289 | 0.0 | 3.289 | 0.0 | 4.877 |
| Al1-S1-Al2 | 26.090 | 117.324 | 1.280 | 1.618 | 0.0 | 3.500 | 0.0 | 3.289 | 0.0 | 4.853 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Al1-S1-S1 | 1.000 | 1.618 | 2.032 | 46.910 | 1.000 | -0.184 | 11.476 | 2.112 | 4 | 0 | 0.0 |
| Al1-Al2-Al2 | 1.000 | 1.280 | 2.735 | 0.000 | 1.000 | 0.000 | 4.575 | 8.388 | 4 | 0 | 0.0 |
| Al1-Al2-S1 | 1.000 | 0.000 | 0.000 | 26.090 | 1.000 | -0.459 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 10.014 | 6.133 | 2.925 | 1.900 |
| or | 2.360 | 2.470 | 100.921 | 117.065 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga1-S1 | 10.825 | 1.658 | 15.510 | 0.0 | 3.349 |
| Ga1-Ga2 | 6.316 | 1.506 | 18.610 | 0.0 | 3.434 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-S1-S1 | 43.355 | 100.921 | 1.658 | 1.658 | 0.0 | 3.349 | 0.0 | 3.349 | 0.0 | 4.972 |
| Ga1-S1-Ga2 | 30.536 | 117.065 | 1.658 | 1.506 | 0.0 | 3.349 | 0.0 | 3.434 | 0.0 | 4.809 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-S1-S1 | 1.000 | 1.658 | 2.020 | 43.355 | 1.000 | -0.189 | 10.825 | 2.052 | 4 | 0 | 0.0 |
| Ga1-Ga2-Ga2 | 1.000 | 1.506 | 2.280 | 0.000 | 1.000 | 0.000 | 6.316 | 3.615 | 4 | 0 | 0.0 |
| Ga1-Ga2-S1 | 1.000 | 0.000 | 0.000 | 30.536 | 1.000 | -0.455 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 10.014 | 4.533 | 2.179 | 1.412 |
| or | 2.560 | 2.820 | 100.624 | 117.305 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In1-S1 | 12.652 | 1.787 | 21.475 | 0.0 | 3.629 |
| In1-In2 | 5.202 | 1.454 | 31.620 | 0.0 | 3.833 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In1-S1-S1 | 31.876 | 100.624 | 1.787 | 1.787 | 0.0 | 3.629 | 0.0 | 3.629 | 0.0 | 5.382 |
| In1-S1-In2 | 19.900 | 117.305 | 1.787 | 1.454 | 0.0 | 3.629 | 0.0 | 3.833 | 0.0 | 5.325 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In1-S1-S1 | 1.000 | 1.787 | 2.031 | 31.876 | 1.000 | -0.184 | 12.652 | 2.108 | 4 | 0 | 0.0 |
| In1-In2-In2 | 1.000 | 1.454 | 2.635 | 0.000 | 1.000 | 0.000 | 5.202 | 7.067 | 4 | 0 | 0.0 |
| In1-In2-S1 | 1.000 | 0.000 | 0.000 | 19.990 | 1.000 | -0.459 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 17.138 | 15.227 | 5.144 | 3.113 |
| or | 2.100 | 1.710 | 101.394 | 116.681 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| B1-Se1 | 14.825 | 1.491 | 9.724 | 0.0 | 2.985 |
| B1-B2 | 17.700 | 2.252 | 4.275 | 0.0 | 2.691 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| B1-S1-Se1 | 77.850 | 101.394 | 1.491 | 1.491 | 0.0 | 2.985 | 0.0 | 2.985 | 0.0 | 4.440 |
| B1-B2-Se1 | 104.372 | 116.681 | 2.252 | 1.491 | 0.0 | 2.691 | 0.0 | 2.985 | 0.0 | 3.923 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| B1-Se1-Se1 | 1.000 | 1.491 | 2.002 | 77.850 | 1.000 | -0.198 | 14.825 | 1.968 | 4 | 0 | 0.0 |
| B1-B2-B2 | 1.000 | 2.252 | 1.195 | 0.000 | 1.000 | 0.000 | 17.700 | 0.166 | 4 | 0 | 0.0 |
| B1-B2-Se1 | 1.000 | 0.000 | 0.000 | 104.372 | 1.000 | -0.449 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.831 | 4.487 | 2.916 | 1.659 |
| or | 2.470 | 2.570 | 99.846 | 117.926 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Al1-Se1 | 11.362 | 1.694 | 18.610 | 0.0 | 3.493 |
| Al1-Al2 | 4.974 | 1.558 | 21.812 | 0.0 | 3.570 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Al1-Se1-Se1 | 41.235 | 99.846 | 1.694 | 1.694 | 0.0 | 3.493 | 0.0 | 3.493 | 0.0 | 5.164 |
| Al1-Se1-Al2 | 26.418 | 117.926 | 1.558 | 1.694 | 0.0 | 3.570 | 0.0 | 3.493 | 0.0 | 5.029 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Al1-Se1-Se1 | 1.000 | 1.694 | 2.062 | 41.235 | 1.000 | -0.171 | 11.362 | 2.260 | 4 | 0 | 0.0 |
| Al1-Al2-Al2 | 1.000 | 1.558 | 2.292 | 0.000 | 1.000 | 0.000 | 4.974 | 3.704 | 4 | 0 | 0.0 |
| Al1-Al2-Se1 | 1.000 | 0.000 | 0.000 | 26.418 | 1.000 | -0.468 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 10.014 | 5.400 | 2.925 | 1.701 |
| or | 2.500 | 2.460 | 99.636 | 118.092 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga1-Se1 | 11.798 | 1.706 | 19.531 | 0.0 | 3.533 |
| Ga1-Ga2 | 6.479 | 1.765 | 18.311 | 0.0 | 3.502 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-Se1-Se1 | 40.978 | 99.636 | 1.706 | 1.706 | 0.0 | 3.533 | 0.0 | 3.533 | 0.0 | 5.218 |
| Ga1-Se1-Ga2 | 31.031 | 118.092 | 1.765 | 1.706 | 0.0 | 3.502 | 0.0 | 3.533 | 0.0 | 4.985 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-Se1-Se1 | 1.000 | 1.706 | 2.070 | 40.978 | 1.000 | -0.167 | 11.798 | 2.305 | 4 | 0 | 0.0 |
| Ga1-Ga2-Ga2 | 1.000 | 1.765 | 1.984 | 0.000 | 1.000 | 0.000 | 6.479 | 1.888 | 4 | 0 | 0.0 |
| Ga1-Ga2-Se1 | 1.000 | 0.000 | 0.000 | 31.031 | 1.000 | -0.471 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 9.812 | 4.185 | 2.090 | 1.227 |
| or | 2.690 | 2.810 | 99.296 | 118.361 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In1-Se1 | 13.281 | 1.822 | 26.181 | 0.0 | 3.797 |
| In1-In2 | 5.414 | 1.661 | 31.174 | 0.0 | 2.890 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In1-Se1-Se1 | 28.853 | 99.296 | 1.822 | 1.822 | 0.0 | 3.797 | 0.0 | 3.797 | 0.0 | 5.601 |
| In1-Se1-In2 | 19.120 | 118.361 | 1.822 | 1.661 | 0.0 | 3.797 | 0.0 | 3.890 | 0.0 | 5.489 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In1-Se1-Se1 | 1.000 | 1.822 | 2.084 | 28.853 | 1.000 | -0.162 | 13.281 | 2.377 | 4 | 0 | 0.0 |
| In1-In2-In2 | 1.000 | 1.661 | 2.342 | 0.000 | 1.000 | 0.000 | 5.414 | 4.094 | 4 | 0 | 0.0 |
| In1-In2-Se1 | 1.000 | 0.000 | 0.000 | 19.120 | 1.000 | -0.475 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 13.287 | 14.502 | 5.466 | 2.515 |
| or | 2.310 | 1.710 | 100.809 | 117.156 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| B1-Te1 | 13.727 | 1.619 | 14.237 | 0.0 | 3.277 |
| B1-B2 | 24.140 | 2.933 | 4.275 | 0.0 | 2.830 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| B1-Te1-Te1 | 80.622 | 100.809 | 1.619 | 1.619 | 0.0 | 3.277 | 0.0 | 3.277 | 0.0 | 4.863 |
| B1-B2-Te1 | 116.3301 | 117.156 | 2.933 | 1.619 | 0.0 | 2.830 | 0.0 | 3.277 | 0.0 | 4.199 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| B1-Te1-Te1 | 1.000 | 1.619 | 2.024 | 80.622 | 1.000 | -0.188 | 13.727 | 2.073 | 4 | 0 | 0.0 |
| B1-B2-B2 | 1.000 | 2.933 | 0.965 | 0.000 | 1.000 | 0.000 | 24.140 | 0.058 | 4 | 0 | 0.0 |
| B1-B2-Te1 | 1.000 | 0.000 | 0.000 | 116.301 | 1.000 | -0.456 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 8.077 | 3.859 | 2.820 | 1.518 |
| or | 2.700 | 2.580 | 99.124 | 118.495 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Al1-Te1 | 10.971 | 1.821 | 26.572 | 0.0 | 3.809 |
| Al1-Al2 | 5.523 | 2.002 | 22.154 | 0.0 | 3.716 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Al1-Te1-Te1 | 38.638 | 99.124 | 1.821 | 1.821 | 0.0 | 3.809 | 0.0 | 3.809 | 0.0 | 5.614 |
| Al1-Te1-Al2 | 29.574 | 118.495 | 2.002 | 1.821 | 0.0 | 3.716 | 0.0 | 3.809 | 0.0 | 5.330 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Al1-Te1-Te1 | 1.000 | 1.821 | 2.091 | 38.638 | 1.000 | -0.159 | 10.971 | 2.415 | 4 | 0 | 0.0 |
| Al1-Al2-Al2 | 1.000 | 2.002 | 1.856 | 0.000 | 1.000 | 0.000 | 5.523 | 1.379 | 4 | 0 | 0.0 |
| Al1-Al2-Te1 | 1.000 | 0.000 | 0.000 | 29.574 | 1.000 | -0.477 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 7.382 | 4.366 | 2.841 | 1.519 |
| or | 2.700 | 2.460 | 99.781 | 117.978 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| Ga1-Te1 | 10.179 | 1.849 | 26.572 | 0.0 | 3.817 |
| Ga1-Ga2 | 6.750 | 2.239 | 18.311 | 0.0 | 3.634 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-Te1-Te1 | 40.060 | 99.781 | 1.849 | 1.849 | 0.0 | 3.817 | 0.0 | 3.817 | 0.0 | 5.642 |
| Ga1-Te1-Ga2 | 34.354 | 117.978 | 2.239 | 1.849 | 0.0 | 3.634 | 0.0 | 3.817 | 0.0 | 5.238 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Ga1-Te1-Te1 | 1.000 | 1.849 | 2.065 | 40.060 | 1.000 | -0.170 | 10.179 | 2.274 | 4 | 0 | 0.0 |
| Ga1-Ga2-Ga2 | 1.000 | 2.239 | 1.623 | 0.000 | 1.000 | 0.000 | 6.750 | 0.728 | 4 | 0 | 0.0 |
| Ga1-Ga2-Te1 | 1.000 | 0.000 | 0.000 | 34.354 | 1.000 | -0.469 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 5.592 | 3.928 | 2.419 | 1.227 |
| or | 2.890 | 2.810 | 99.148 | 118.477 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| In1-Te1 | 8.707 | 1.950 | 34.879 | 0.0 | 4.077 |
| In1-In2 | 6.312 | 2.068 | 31.174 | 0.0 | 4.015 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| In1-Te1-Te1 | 33.178 | 99.148 | 1.950 | 1.950 | 0.0 | 4.077 | 0.0 | 4.077 | 0.0 | 6.011 |
| In1-Te1-In2 | 22.833 | 118.477 | 2.068 | 1.950 | 0.0 | 4.015 | 0.0 | 4.077 | 0.0 | 5.741 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| In1-Te1-Te1 | 1.000 | 1.950 | 2.090 | 33.178 | 1.000 | -0.159 | 8.707 | 2.410 | 4 | 0 | 0.0 |
| In1-In2-In2 | 1.000 | 2.068 | 1.942 | 0.000 | 1.000 | 0.000 | 6.312 | 1.704 | 4 | 0 | 0.0 |
| In1-In2-Te1 | 1.000 | 0.000 | 0.000 | 22.833 | 1.000 | -0.477 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| VFF type | bond stretching | angle bending | ||
|---|---|---|---|---|
| expression | ||||
| parameter | 20.673 | 6.025 | 3.523 | 4.651 |
| or | 1.614 | 1.880 | 64.581 | 99.318 |
| (eV) | (Å) | (Å4) | (Å) | ||
|---|---|---|---|---|---|
| 8.974 | 0.971 | 3.393 | 0.0 | 2.240 | |
| 2.098 | 0.618 | 6.246 | 0.0 | 2.419 |
| (eV) | (degree) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | (Å) | |
|---|---|---|---|---|---|---|---|---|---|---|
| 32.074 | 64.581 | 0.971 | 0.618 | 0.0 | 2.240 | 0.0 | 2.419 | 0.0 | 2.419 | |
| 23.668 | 99.318 | 0.618 | 0.618 | 0.0 | 2.419 | 0.0 | 2.410 | 2.240 | 3.047 |
| (eV) | (Å) | tol | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| B1-B5-B5 | 1.000 | 0.971 | 2.307 | 0.000 | 1.000 | 0.000 | 8.974 | 3.817 | 4 | 0 | 0.0 |
| B1-B2-B2 | 1.000 | 0.618 | 3.914 | 0.000 | 1.000 | 0.000 | 2.098 | 42.820 | 4 | 0 | 0.0 |
| B1-B2-B5 | 1.000 | 0.000 | 0.000 | 32.074 | 1.000 | 0.429 | 0.000 | 0.000 | 4 | 0 | 0.0 |
| B1-B2-B4 | 1.000 | 0.000 | 0.000 | 23.668 | 1.000 | -0.162 | 0.000 | 0.000 | 4 | 0 | 0.0 |
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Parameterization of Stillinger-Weber Potential for Two-Dimensional Atomic Crystals
Jin-Wu Jiang
Corresponding author: [email protected]; [email protected]
Shanghai Institute of Applied Mathematics and Mechanics, Shanghai Key Laboratory of Mechanics in Energy Engineering, Shanghai University, Shanghai 200072, People’s Republic of China
Yu-Ping Zhou
Shanghai Institute of Applied Mathematics and Mechanics, Shanghai Key Laboratory of Mechanics in Energy Engineering, Shanghai University, Shanghai 200072, People’s Republic of China
Abstract
We parametrize the Stillinger-Weber potential for 156 two-dimensional atomic crystals. Parameters for the Stillinger-Weber potential are obtained from the valence force field model following the analytic approach (Nanotechnology 26, 315706 (2015)), in which the valence force constants are determined by the phonon spectrum. The Stillinger-Weber potential is an efficient nonlinear interaction, and is applicable for numerical simulations of nonlinear physical or mechanical processes. The supplemental resources for all simulations in the present work are available online in Ref. Jia, , including a fortran code to generate crystals’ structures, files for molecular dynamics simulations using LAMMPS, files for phonon calculations with the Stillinger-Weber potential using GULP, and files for phonon calculations with the valence force field model using GULP.
Layered Crystal, Stillinger-Weber Potential, Molecular Dynamics Simulation, Empirical Potential
pacs:
78.20.Bh, 63.22.-m, 62.25.-g
I Introduction
The atomic interaction is of essential importance in the numerical investigation of most physical or mechanical processes. The present work provides parameters for the Stillinger-Weber (SW) empirical potential for 156 two-dimensional atomic crystal (TDACs). In practical applications, these layered materials are usually played as lego on atomic scale to construct the van der Waals heterostructures with comprehensive properties.Geim and Grigorieva (2013) The computational cost of ab initio for the heterostructure will be substantially increased as compared with one individual atomic layer, because the unit cell for the heterostructure is typically very large resulting from the mismatch of the lattice constants of different layered components. The empirical potential will be a competitive alternative to help out this difficult situation, considering their high efficiency.
In the early stage before 1980s, the computation ability of the scientific community was quite limited. At that time, the valence force field (VFF) model was one popular empirical potential for the description of the atomic interaction, since the VFF model is linear and can be applied in the analytic derivation of most elastic quantities.Yu (2010) In this model, each VFF term corresponds to a particular motion style in the crystal. Hence, each parameter in the VFF model usually has clear physical essence, which is beneficial for the parameterization of this model. For instance, the bond stretching term in the VFF model is directly related to the frequency of the longitudinal optical phonon modes, so the force constant of the bond stretching term can be determined from the frequencies of the longitudinal optical phonon modes. The VFF model can thus serve as the starting point for developing atomic empirical potentials for different crystals.
While the VFF model is beneficial for the fastest numerical simulation, its strong limitation is the absence of nonlinear effect. Due to this limitation, the VFF model is not applicable to nonlinear phenomena, for which other potential models with nonlinear components are required. Some representative potential models are (in the order of their simulation costs) SW potential,Stillinger and Weber (1985) Tersoff potential,Tersoff (1986) Brenner potential,Brenner et al. (2002) ab initio approaches, and etc. The SW potential is one of the simplest potential forms with nonlinear effects included. An advanced feature for the SW potential is that it includes the nonlinear effect, and keeps the numerical simulation at a very fast level.
Considering its distinct advantages, the present article aims at providing the SW potential for 156 TDACs. We will determine parameters for the SW potential from the VFF model, following the analytic approach proposed by one of the present author (J.W.J).Jiang (2015a) The VFF constants are fitted to the phonon spectrum or the elastic properties in the TDACs.
In this paper, we parametrize the SW potential for 156 TDACs. All structures discussed in the present work are listed in Tables 1, 2, 3, 4, 5, 6, 7, 8, and 9. The supplemental materials are freely available online in Ref. Jia, , including a fortran code to generate crystals’ structures, files for molecular dynamics simulations using LAMMPS, files for phonon calculations with the SW potential using GULP, and files for phonon calculations with the valence force field model using GULP.
II VFF model and SW potential
II.1 VFF model
The VFF model is one of the most widely used linear model for the description of atomic interactions.Yu (2010) The bond stretching and the angle bending are two typical motion styles for most covalent bonding materials. The bond stretching describes the energy variation for a bond due to a bond variation , with as the initial bond length. The angle bending gives the energy increment for an angle resulting from an angle variation , with as the initial angle. In the VFF model, the energy variations for the bond stretching and the angle bending are described by the following quadratic forms,
[TABLE]
where and are two force constant parameters. These two potential expressions in Eqs. (1) and (2) are directly related to the optical phonon modes in the crystal. Hence, their force constant parameters and are usually determined by fitting to the phonon dispersion.
II.2 SW potential
In the SW potential, energy increments for the bond stretching and angle bending are described by the following two-body and three-body forms,
[TABLE]
where corresponds to the bond stretching and associates with the angle bending. The cut-offs , and are geometrically determined by the material’s structure. There are five unknown geometrical parameters, i.e., and in the two-body term and , , and in the three-body term, and two energy parameters and . There is a constraint among these parameters due to the equilibrium condition,Jiang (2015a)
[TABLE]
where is the equilibrium bond length from experiments. Eq. (5) ensures that the bond has an equilibrium length of and the interaction for this bond is at the energy minimum state at the equilibrium configuration.
The energy parameters and in the SW potential can be analytically derived from the VFF model as follows,
[TABLE]
where the coefficient in Eq. (6) is,
[TABLE]
In some situations, the SW potential is also written into the following form,
[TABLE]
The parameters here can be determined by comparing the SW potential forms in Eqs. (9) and (10) with Eqs. (3) and (4). It is obvious that and . Eqs. (9) and (10) have two more parameters than Eqs. (3) and (4), so we can set eV and . The other parameters in Eqs. (9) and (10) are related to these parameters in Eqs. (3) and (4) by the following equations
[TABLE]
The SW potential is implemented in GULP using Eqs. (3) and (4). The SW potential is implemented in LAMMPS using Eqs. (9) and (10).
In the rest of this article, we will develop the VFF model and the SW potential for layered crystals. The VFF model will be developed by fitting to the phonon dispersion from experiments or first-principles calculations. The SW potential will be developed following the above analytic parameterization approach. In this work, GULPGale (1997) is used for the calculation of phonon dispersion and the fitting process, while LAMMPSlammps (2012) is used for molecular dynamics simulations. The OVITOStukowski (2010) and XCRYSDENKokalj (2003) packages are used for visualization. All simulation scripts for GULP and LAMMPS are available online in Ref. Jia, .
III 1H-ScO2
Most existing theoretical studies on the single-layer 1H-ScO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-ScO2.
The structure for the single-layer 1H-ScO2 is shown in Fig. 1 (with M=Sc and X=O). Each Sc atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 10 shows four VFF terms for the single-layer 1H-ScO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along M as shown in Fig. 3 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 3 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 11. The parameters for the three-body SW potential used by GULP are shown in Tab. 12. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 13. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-ScO2 using LAMMPS, because the angles around atom Sc in Fig. 1 (with M=Sc and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Sc and X=O) shows that, for 1H-ScO2, we can differentiate these angles around the Sc atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Sc atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-ScO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 4 shows the stress-strain curve for the tension of a single-layer 1H-ScO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-ScO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-ScO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 126.3 N/m and 125.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-ScO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -652.8 N/m and -683.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.2 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.7 Nm*-1* at the ultimate strain of 0.23 in the zigzag direction at the low temperature of 1 K.
IV 1H-ScS2
Most existing theoretical studies on the single-layer 1H-ScS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-ScS2.
The structure for the single-layer 1H-ScS2 is shown in Fig. 1 (with M=Sc and X=S). Each Sc atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 14 shows four VFF terms for the single-layer 1H-ScS2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 5 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 5 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 15. The parameters for the three-body SW potential used by GULP are shown in Tab. 16. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 17. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-ScS2 using LAMMPS, because the angles around atom Sc in Fig. 1 (with M=Sc and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Sc and X=S) shows that, for 1H-ScS2, we can differentiate these angles around the Sc atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Sc atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-ScS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 6 shows the stress-strain curve for the tension of a single-layer 1H-ScS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-ScS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-ScS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 43.8 N/m and 43.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-ScS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -146.9 N/m and -159.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.32 in the zigzag direction at the low temperature of 1 K.
V 1H-ScSe2
Most existing theoretical studies on the single-layer 1H-ScSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-ScSe2.
The structure for the single-layer 1H-ScSe2 is shown in Fig. 1 (with M=Sc and X=Se). Each Sc atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 18 shows four VFF terms for the single-layer 1H-ScSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 7 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 7 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 19. The parameters for the three-body SW potential used by GULP are shown in Tab. 20. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 21. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-ScSe2 using LAMMPS, because the angles around atom Sc in Fig. 1 (with M=Sc and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Sc and X=Se) shows that, for 1H-ScSe2, we can differentiate these angles around the Sc atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Sc atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-ScSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 8 shows the stress-strain curve for the tension of a single-layer 1H-ScSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-ScSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-ScSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 39.4 N/m and 39.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-ScSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -115.7 N/m and -135.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.35 in the zigzag direction at the low temperature of 1 K.
VI 1H-ScTe2
Most existing theoretical studies on the single-layer 1H-ScTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-ScTe2.
The structure for the single-layer 1H-ScTe2 is shown in Fig. 1 (with M=Sc and X=Te). Each Sc atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 22 shows four VFF terms for the single-layer 1H-ScTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 9 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. There is only one (longitudinal) acoustic branch available. We find that the VFF parameters can be chosen to be the same as that of the 1H-ScSe2, from which the longitudinal acoustic branch agrees with the ab initio results as shown in Fig. 9 (a). It has also been shown that the VFF parameters can be the same for TaSe2 and NbSe2 of similar structure.Feldman (1982) Fig. 9 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 23. The parameters for the three-body SW potential used by GULP are shown in Tab. 24. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 25. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-ScTe2 using LAMMPS, because the angles around atom Sc in Fig. 1 (with M=Sc and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Sc and X=Te) shows that, for 1H-ScTe2, we can differentiate these angles around the Sc atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Sc atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-ScTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 10 shows the stress-strain curve for the tension of a single-layer 1H-ScTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-ScTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-ScTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 29.3 N/m and 28.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-ScTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -43.2 N/m and -59.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.7 Nm*-1* at the ultimate strain of 0.33 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.7 Nm*-1* at the ultimate strain of 0.45 in the zigzag direction at the low temperature of 1 K.
VII 1H-TiTe2
Most existing theoretical studies on the single-layer 1H-TiTe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-TiTe2.
The structure for the single-layer 1H-TiTe2 is shown in Fig. 1 (with M=Ti and X=Se). Each Ti atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ti atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 26 shows the VFF terms for the 1H-TiTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 11 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 11 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 27. The parameters for the three-body SW potential used by GULP are shown in Tab. 28. Parameters for the SW potential used by LAMMPS are listed in Tab. 29. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-TiTe2 using LAMMPS, because the angles around atom Ti in Fig. 1 (with M=Ti and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ti and X=Te) shows that, for 1H-TiTe2, we can differentiate these angles around the Ti atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ti atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-TiTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 12 shows the stress-strain curve for the tension of a single-layer 1H-TiTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-TiTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-TiTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 47.9 N/m and 47.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-TiTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -158.6 N/m and -176.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.6 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.3 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
VIII 1H-VO2
Most existing theoretical studies on the single-layer 1H-VO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-VO2.
The structure for the single-layer 1H-VO2 is shown in Fig. 1 (with M=V and X=O). Each V atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three V atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 30 shows four VFF terms for the single-layer 1H-VO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 13 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 13 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 31. The parameters for the three-body SW potential used by GULP are shown in Tab. 32. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 33. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-VO2 using LAMMPS, because the angles around atom V in Fig. 1 (with M=V and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=V and X=O) shows that, for 1H-VO2, we can differentiate these angles around the V atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one V atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-VO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 14 shows the stress-strain curve for the tension of a single-layer 1H-VO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-VO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-VO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 133.0 N/m and 132.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-VO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -652.3 N/m and -705.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 13.3 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.7 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
IX 1H-VS2
Most existing theoretical studies on the single-layer 1H-VS2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-VS2.
The structure for the single-layer 1H-VS2 is shown in Fig. 1 (with M=V and X=S). Each V atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three V atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 34 shows the VFF terms for the 1H-VS2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 15 (a). The ab initio calculations for the phonon dispersion are from Ref. Isaacs and Marianetti, 2016. The phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012) Fig. 15 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 35. The parameters for the three-body SW potential used by GULP are shown in Tab. 36. Parameters for the SW potential used by LAMMPS are listed in Tab. 37. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-VS2 using LAMMPS, because the angles around atom V in Fig. 1 (with M=V and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=V and X=S) shows that, for 1H-VS2, we can differentiate these angles around the V atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one V atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-VS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 16 shows the stress-strain curve for the tension of a single-layer 1H-VS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-VS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-VS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 86.5 N/m and 85.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-VS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -302.0 N/m and -334.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.5 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.9 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
X 1H-VSe2
Most existing theoretical studies on the single-layer 1H-VSe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-VSe2.
The structure for the single-layer 1H-VSe2 is shown in Fig. 1 (with M=V and X=Se). Each V atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three V atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 38 shows the VFF terms for the 1H-VSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 17 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 17 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 39. The parameters for the three-body SW potential used by GULP are shown in Tab. 40. Parameters for the SW potential used by LAMMPS are listed in Tab. 41. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-VSe2 using LAMMPS, because the angles around atom V in Fig. 1 (with M=V and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=V and X=Se) shows that, for 1H-VSe2, we can differentiate these angles around the V atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one V atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-VSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 18 shows the stress-strain curve for the tension of a single-layer 1H-VSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-VSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-VSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 81.7 N/m and 80.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-VSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -335.2 N/m and -363.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.5 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
XI 1H-VTe2
Most existing theoretical studies on the single-layer 1H-VTe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-VTe2.
The structure for the single-layer 1H-VTe2 is shown in Fig. 1 (with M=V and X=Te). Each V atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three V atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 42 shows the VFF terms for the 1H-VTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 19 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 19 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 43. The parameters for the three-body SW potential used by GULP are shown in Tab. 44. Parameters for the SW potential used by LAMMPS are listed in Tab. 45. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-VTe2 using LAMMPS, because the angles around atom V in Fig. 1 (with M=V and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=V and X=Te) shows that, for 1H-VTe2, we can differentiate these angles around the V atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one V atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-VTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 20 shows the stress-strain curve for the tension of a single-layer 1H-VTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-VTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-VTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 68.1 N/m and 66.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-VTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -237.4 N/m and -260.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
XII 1H-CrO2
Most existing theoretical studies on the single-layer 1H-CrO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-CrO2.
The structure for the single-layer 1H-CrO2 is shown in Fig. 1 (with M=Cr and X=O). Each Cr atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Cr atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 46 shows four VFF terms for the single-layer 1H-CrO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 21 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 21 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 47. The parameters for the three-body SW potential used by GULP are shown in Tab. 48. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 49. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-CrO2 using LAMMPS, because the angles around atom Cr in Fig. 1 (with M=Cr and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Cr and X=O) shows that, for 1H-CrO2, we can differentiate these angles around the Cr atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Cr atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-CrO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 22 shows the stress-strain curve for the tension of a single-layer 1H-CrO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-CrO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-CrO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 210.6 N/m and 209.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-CrO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -1127.7 N/m and -1185.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 19.4 Nm*-1* at the ultimate strain of 0.18 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 18.7 Nm*-1* at the ultimate strain of 0.20 in the zigzag direction at the low temperature of 1 K.
XIII 1H-CrS2
Most existing theoretical studies on the single-layer 1H-CrS2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-CrS2.
The structure for the single-layer 1H-CrS2 is shown in Fig. 1 (with M=Cr and X=S). Each Cr atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Cr atoms. The structural parameters are from Ref. Zhuang et al., 2014, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 50 shows four VFF terms for the 1H-CrS2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 23 (a). The ab initio calculations for the phonon dispersion are from Ref. Zhuang et al., 2014. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012) Fig. 23 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 51. The parameters for the three-body SW potential used by GULP are shown in Tab. 52. Parameters for the SW potential used by LAMMPS are listed in Tab. 53. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-CrS2 using LAMMPS, because the angles around atom Cr in Fig. 1 (with M=Cr and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Cr and X=S) shows that, for 1H-CrS2, we can differentiate these angles around the Cr atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Cr atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-CrS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 24 shows the stress-strain curve for the tension of a single-layer 1H-CrS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-CrS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-CrS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 98.4 N/m and 97.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 112.0 N/m from Refs Cakir, Peeters, and Sevik, 2014, or 111.9 N/m from Ref. Alyoruk et al., 2015. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.27.Cakir, Peeters, and Sevik (2014); Alyoruk et al. (2015)
There is no available value for the nonlinear quantities in the single-layer 1H-CrS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -364.8 N/m and -409.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.4 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.8 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
XIV 1H-CrSe2
Most existing theoretical studies on the single-layer 1H-CrSe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-CrSe2.
The structure for the single-layer 1H-CrSe2 is shown in Fig. 1 (with M=Cr and X=Se). Each Cr atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Cr atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 54 shows four VFF terms for the 1H-CrSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 25 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 25 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 55. The parameters for the three-body SW potential used by GULP are shown in Tab. 56. Parameters for the SW potential used by LAMMPS are listed in Tab. 57. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-CrSe2 using LAMMPS, because the angles around atom Cr in Fig. 1 (with M=Cr and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Cr and X=Se) shows that, for 1H-CrSe2, we can differentiate these angles around the Cr atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Cr atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-CrSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 26 shows the stress-strain curve for the tension of a single-layer 1H-CrSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-CrSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-CrSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 90.0 N/m and 89.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 88.0 N/m from Refs Cakir, Peeters, and Sevik, 2014, or 87.9 N/m from Ref. Alyoruk et al., 2015. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.30.Cakir, Peeters, and Sevik (2014); Alyoruk et al. (2015)
There is no available value for the nonlinear quantities in the single-layer 1H-CrSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most two-dimensional atomic layered materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -279.6 N/m and -318.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 13.0 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.4 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XV 1H-CrTe2
Most existing theoretical studies on the single-layer 1H-CrTe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-CrTe2.
The structure for the single-layer 1H-CrTe2 is shown in Fig. 1 (with M=Cr and X=Te). Each Cr atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Cr atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 58 shows three VFF terms for the 1H-CrTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 27 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 27 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 59. The parameters for the three-body SW potential used by GULP are shown in Tab. 60. Parameters for the SW potential used by LAMMPS are listed in Tab. 61. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-CrTe2 using LAMMPS, because the angles around atom Cr in Fig. 1 (with M=Cr and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Cr and X=Te) shows that, for 1H-CrTe2, we can differentiate these angles around the Cr atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Cr atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-CrTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 28 shows the stress-strain curve for the tension of a single-layer 1H-CrTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-CrTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-CrTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 77.2 N/m and 76.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 63.9 N/m from Refs Cakir, Peeters, and Sevik, 2014 and Alyoruk et al., 2015. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.30.Cakir, Peeters, and Sevik (2014); Alyoruk et al. (2015)
There is no available value for the nonlinear quantities in the single-layer 1H-CrTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most two-dimensional atomic layered materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -237.1 N/m and -280.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.2 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.7 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XVI 1H-MnO2
Most existing theoretical studies on the single-layer 1H-MnO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-MnO2.
The structure for the single-layer 1H-MnO2 is shown in Fig. 1 (with M=Mn and X=O). Each Mn atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Mn atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 62 shows four VFF terms for the single-layer 1H-MnO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 29 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Typically, the transverse acoustic branch has a linear dispersion, so is higher than the flexural branch. However, it can be seen that the transverse acoustic branch is close to the flexural branch, which should be due to the underestimation from the ab initio calculations. Fig. 29 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 63. The parameters for the three-body SW potential used by GULP are shown in Tab. 64. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 65. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-MnO2 using LAMMPS, because the angles around atom Mn in Fig. 1 (with M=Mn and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Mn and X=O) shows that, for 1H-MnO2, we can differentiate these angles around the Mn atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Mn atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-MnO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 30 shows the stress-strain curve for the tension of a single-layer 1H-MnO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-MnO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-MnO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 161.1 N/m and 160.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-MnO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -915.9 N/m and -957.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 14.1 Nm*-1* at the ultimate strain of 0.17 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 13.7 Nm*-1* at the ultimate strain of 0.20 in the zigzag direction at the low temperature of 1 K.
XVII 1H-FeO2
Most existing theoretical studies on the single-layer 1H-FeO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-FeO2.
The structure for the single-layer 1H-FeO2 is shown in Fig. 1 (with M=Fe and X=O). Each Fe atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Fe atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 66 shows four VFF terms for the single-layer 1H-FeO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 31 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 31 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 67. The parameters for the three-body SW potential used by GULP are shown in Tab. 68. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 69. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-FeO2 using LAMMPS, because the angles around atom Fe in Fig. 1 (with M=Fe and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Fe and X=O) shows that, for 1H-FeO2, we can differentiate these angles around the Fe atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Fe atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-FeO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 32 shows the stress-strain curve for the tension of a single-layer 1H-FeO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-FeO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-FeO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 100.2 N/m and 99.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-FeO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -423.4 N/m and -460.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.4 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.9 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XVIII 1H-FeS2
Most existing theoretical studies on the single-layer 1H-FeS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-FeS2.
The structure for the single-layer 1H-FeS2 is shown in Fig. 1 (with M=Fe and X=S). Each Fe atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Fe atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 70 shows four VFF terms for the single-layer 1H-FeS2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 33 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 33 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 71. The parameters for the three-body SW potential used by GULP are shown in Tab. 72. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 73. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-FeS2 using LAMMPS, because the angles around atom Fe in Fig. 1 (with M=Fe and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Fe and X=S) shows that, for 1H-FeS2, we can differentiate these angles around the Fe atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Fe atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-FeS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 34 shows the stress-strain curve for the tension of a single-layer 1H-FeS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-FeS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-FeS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 83.6 N/m and 83.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-FeS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -377.5 N/m and -412.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.23 in the zigzag direction at the low temperature of 1 K.
XIX 1H-FeSe2
Most existing theoretical studies on the single-layer 1H-FeSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-FeSe2.
The structure for the single-layer 1H-FeSe2 is shown in Fig. 1 (with M=Fe and X=Se). Each Fe atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Fe atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 74 shows four VFF terms for the single-layer 1H-FeSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 35 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 35 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 75. The parameters for the three-body SW potential used by GULP are shown in Tab. 76. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 77. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-FeSe2 using LAMMPS, because the angles around atom Fe in Fig. 1 (with M=Fe and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Fe and X=Se) shows that, for 1H-FeSe2, we can differentiate these angles around the Fe atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Fe atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-FeSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 36 shows the stress-strain curve for the tension of a single-layer 1H-FeSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-FeSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-FeSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 77.3 N/m and 77.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-FeSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -323.8 N/m and -360.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.8 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.4 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XX 1H-FeTe2
Most existing theoretical studies on the single-layer 1H-FeTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-FeTe2.
The structure for the single-layer 1H-FeTe2 is shown in Fig. 1 (with M=Fe and X=Te). Each Fe atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Fe atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 78 shows four VFF terms for the single-layer 1H-FeTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 37 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 37 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 79. The parameters for the three-body SW potential used by GULP are shown in Tab. 80. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 81. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-FeTe2 using LAMMPS, because the angles around atom Fe in Fig. 1 (with M=Fe and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Fe and X=Te) shows that, for 1H-FeTe2, we can differentiate these angles around the Fe atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Fe atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-FeTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 38 shows the stress-strain curve for the tension of a single-layer 1H-FeTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-FeTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-FeTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 69.6 N/m and 69.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-FeTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -267.5 N/m and -302.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.1 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
XXI 1H-CoTe2
Most existing theoretical studies on the single-layer 1H-CoTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-CoTe2.
The structure for the single-layer 1H-CoTe2 is shown in Fig. 1 (with M=Co and X=Te). Each Co atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Co atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 82 shows four VFF terms for the single-layer 1H-CoTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 39 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 39 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 83. The parameters for the three-body SW potential used by GULP are shown in Tab. 84. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 85. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-CoTe2 using LAMMPS, because the angles around atom Co in Fig. 1 (with M=Co and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Co and X=Te) shows that, for 1H-CoTe2, we can differentiate these angles around the Co atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Co atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-CoTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 40 shows the stress-strain curve for the tension of a single-layer 1H-CoTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-CoTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-CoTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 53.7 N/m and 54.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-CoTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -157.2 N/m and -187.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.2 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.9 Nm*-1* at the ultimate strain of 0.33 in the zigzag direction at the low temperature of 1 K.
XXII 1H-NiS2
Most existing theoretical studies on the single-layer 1H-NiS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-NiS2.
The structure for the single-layer 1H-NiS2 is shown in Fig. 1 (with M=Ni and X=S). Each Ni atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 86 shows four VFF terms for the single-layer 1H-NiS2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 41 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 41 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 87. The parameters for the three-body SW potential used by GULP are shown in Tab. 88. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 89. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-NiS2 using LAMMPS, because the angles around atom Ni in Fig. 1 (with M=Ni and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ni and X=S) shows that, for 1H-NiS2, we can differentiate these angles around the Ni atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ni atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-NiS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 42 shows the stress-strain curve for the tension of a single-layer 1H-NiS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-NiS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-NiS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 84.0 N/m and 82.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-NiS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -403.2 N/m and -414.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.7 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.3 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
XXIII 1H-NiSe2
Most existing theoretical studies on the single-layer 1H-NiSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-NiSe2.
The structure for the single-layer 1H-NiSe2 is shown in Fig. 1 (with M=Ni and X=Se). Each Ni atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 90 shows four VFF terms for the single-layer 1H-NiSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 43 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 43 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 91. The parameters for the three-body SW potential used by GULP are shown in Tab. 92. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 93. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-NiSe2 using LAMMPS, because the angles around atom Ni in Fig. 1 (with M=Ni and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ni and X=Se) shows that, for 1H-NiSe2, we can differentiate these angles around the Ni atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ni atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-NiSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 44 shows the stress-strain curve for the tension of a single-layer 1H-NiSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-NiSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-NiSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 47.6 N/m and 47.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-NiSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -173.9 N/m and -197.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
XXIV 1H-NiTe2
Most existing theoretical studies on the single-layer 1H-NiTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-NiTe2.
The structure for the single-layer 1H-NiTe2 is shown in Fig. 1 (with M=Ni and X=Te). Each Ni atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 94 shows four VFF terms for the single-layer 1H-NiTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 45 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) The transverse acoustic branch is very close to the longitudinal acoustic branch in the ab initio calculations. Fig. 45 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 95. The parameters for the three-body SW potential used by GULP are shown in Tab. 96. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 97. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-NiTe2 using LAMMPS, because the angles around atom Ni in Fig. 1 (with M=Ni and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ni and X=Te) shows that, for 1H-NiTe2, we can differentiate these angles around the Ni atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ni atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-NiTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 46 shows the stress-strain curve for the tension of a single-layer 1H-NiTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-NiTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-NiTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 53.2 N/m and 53.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-NiTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -156.6 N/m and -184.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.1 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.8 Nm*-1* at the ultimate strain of 0.33 in the zigzag direction at the low temperature of 1 K.
XXV 1H-NbS2
In 1983, the VFF model was developed to investigate the lattice dynamical properties in the bulk 2H-NbS2.FlcMullan (1983) In this section, we will develop the SW potential for the single-layer 1H-NbS2.
The structure for the single-layer 1H-NbS2 is shown in Fig. 1 (with M=Nb and X=S). Each Nb atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Nb atoms. The structural parameters are from Ref. FlcMullan, 1983, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 98 shows four VFF terms for the 1H-NbS2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 47 (a). The theoretical phonon frequencies (gray pentagons) are from Ref. FlcMullan, 1983, which are the phonon dispersion of bulk 2H-NbS2. We have used these phonon frequencies as the phonon dispersion of the single-layer 1H-NbS2, as the inter-layer interaction in the bulk 2H-NbS2 only induces weak effects on the two inplane acoustic branches. The inter-layer coupling will strengthen the out-of-plane acoustic branch (flexural branch), so the flexural branch from the present VFF model (blue line) is lower than the theoretical results for bulk 2H-NbS2 (gray pentagons). Fig. 47 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 99. The parameters for the three-body SW potential used by GULP are shown in Tab. 100. Parameters for the SW potential used by LAMMPS are listed in Tab. 101. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-NbS2 using LAMMPS, because the angles around atom Nb in Fig. 1 (with M=Nb and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Nb and X=S) shows that, for 1H-NbS2, we can differentiate these angles around the Nb atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Nb atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-NbS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 48 shows the stress-strain curve for the tension of a single-layer 1H-NbS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-NbS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-NbS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 87.7 N/m and 87.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-NbS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -315.3 N/m and -355.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.4 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
XXVI 1H-NbSe2
In 1983, the VFF model was developed to investigate the lattice dynamical properties in the bulk 2H-NbSe2.Feldman (1982); FlcMullan (1983) In this section, we will develop the SW potential for the single-layer 1H-NbSe2.
The structure for the single-layer 1H-NbSe2 is shown in Fig. 1 (with M=Nb and X=Se). Each Nb atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Nb atoms. The structural parameters are from Ref. FlcMullan, 1983, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 102 shows four VFF terms for the 1H-NbSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 49 (a). The theoretical phonon frequencies (gray pentagons) are from Ref. FlcMullan, 1983, which are the phonon dispersion of bulk 2H-NbSe2. We have used these phonon frequencies as the phonon dispersion of the single-layer 1H-NbSe2, as the inter-layer interaction in the bulk 2H-NbSe2 only induces weak effects on the two inplane acoustic branches. The inter-layer coupling will strengthen the out-of-plane acoustic branch (flexural branch), so the flexural branch from the present VFF model (blue line) is lower than the theoretical results for bulk 2H-NbSe2 (gray pentagons). It turns out that the VFF parameters for the single-layer 1H-NbSe2 are the same as the single-layer NbS2. The phonon dispersion for single-layer 1H-NbSe2 was also shown in Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 49 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 103. The parameters for the three-body SW potential used by GULP are shown in Tab. 104. Parameters for the SW potential used by LAMMPS are listed in Tab. 105. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-NbSe2 using LAMMPS, because the angles around atom Nb in Fig. 1 (with M=Nb and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Nb and X=Se) shows that, for 1H-NbSe2, we can differentiate these angles around the Nb atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Nb atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-NbSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 50 shows the stress-strain curve for the tension of a single-layer 1H-NbSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-NbSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-NbSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 80.2 N/m and 80.7 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-NbSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -258.8 N/m and -306.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.2 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.7 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
XXVII 1H-MoO2
Most existing theoretical studies on the single-layer 1H-MoO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-MoO2.
The structure for the single-layer 1H-MoO2 is shown in Fig. 1 (with M=Mo and X=O). Each Mo atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Mo atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 106 shows four VFF terms for the single-layer 1H-MoO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 51 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 51 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 107. The parameters for the three-body SW potential used by GULP are shown in Tab. 108. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 109. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-MoO2 using LAMMPS, because the angles around atom Mo in Fig. 1 (with M=Mo and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Mo and X=O) shows that, for 1H-MoO2, we can differentiate these angles around the Mo atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Mo atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-MoO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 52 shows the stress-strain curve for the tension of a single-layer 1H-MoO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-MoO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-MoO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 210.0 N/m and 209.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-MoO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -1027.8 N/m and -1106.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 21.0 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 20.1 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
XXVIII 1H-MoS2
Several potentials have been proposed to describe the interaction for the single-layer 1H-MoS2. In 1975, Wakabayashi et al. developed a VFF model to calculate the phonon spectrum of the bulk 2H-MoS2.Wakabayashi, Smith, and Nicklow (1975) In 2009, Liang et al. parameterized a bond-order potential for 1H-MoS2,Liang, Phillpot, and Sinnott (2009) which is based on the bond order concept underlying the Brenner potential.Brenner et al. (2002) A separate force field model was parameterized in 2010 for MD simulations of bulk 2H-MoS2.Varshney et al. (2010) The present author (J.W.J.) and his collaborators parameterized the SW potential for 1H-MoS2 in 2013,Jiang, Park, and Rabczuk (2013) which was improved by one of the present author (J.W.J.) in 2015.Jiang (2015a) Recently, another set of parameters for the SW potential were proposed for the single-layer 1H-MoS2.Kandemir et al. (2016)
We show the VFF model and the SW potential for single-layer 1H-MoS2 in this section. These potentials have been developed in previous works. The VFF model presented here is from Ref. Wakabayashi, Smith, and Nicklow, 1975, while the SW potential presented in this section is from Ref. Jiang, 2015a.
The structural parameters for the single-layer 1H-MoS2 are from the first-principles calculations as shown in Fig. 1 (with M=Mo and X=S).Molina-Sánchez and Wirtz (2011) The Mo atom layer in the single-layer 1H-MoS2 is sandwiched by two S atom layers. Accordingly, each Mo atom is surrounded by six S atoms, while each S atom is connected to three Mo atoms. The bond length between neighboring Mo and S atoms is Å, and the angles are and .
The VFF model for single-layer 1H-MoS2 is from Ref. Wakabayashi, Smith, and Nicklow, 1975, which is able to describe the phonon spectrum and the sound velocity accurately. We have listed the first three leading force constants for single-layer 1H-MoS2 in Tab. 110, neglecting other weak interaction terms. The SW potential parameters for single-layer 1H-MoS2 used by GULP are listed in Tabs. 111 and 112. The SW potential parameters for single-layer 1H-MoS2 used by LAMMPSlammps (2012) are listed in Tab. 113. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-MoS2 using LAMMPS, because the angles around atom Mo in Fig. 1 (with M=Mo and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Mo and X=S) shows that, for 1H-MoS2, we can differentiate these angles around the Mo atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Mo atom.
We use GULP to compute the phonon dispersion for the single-layer 1H-MoS2 as shown in Fig. 53. The results from the VFF model are quite comparable with the experiment data. The phonon dispersion from the SW potential is the same as that from the VFF model, which indicates that the SW potential has fully inherited the linear portion of the interaction from the VFF model.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-MoS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 54 shows the stress-strain curve during the tension of a single-layer 1H-MoS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-MoS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-MoS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 97 N/m and 96 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is isotropic in the armchair and zigzag directions. These values are in considerable agreement with the experimental results, eg. N/m from Refs Cooper et al., 2013a, b, or N/m from Ref. Bertolazzi, Brivio, and Kis, 2011. The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -418 N/m and -461 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
XXIX 1H-MoSe2
There is a recent parameter set for the SW potential in the single-layer 1H-MoSe2.Kandemir et al. (2016) In this section, we will develop both VFF model and the SW potential for the single-layer 1H-MoSe2.
The structure for the single-layer 1H-MoSe2 is shown in Fig. 1 (with M=Mo and X=Se). Each Mo atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Mo atoms. The structural parameters are from Ref. Horzum et al., 2013, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 114 shows four VFF terms for the 1H-MoSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 55 (a). The ab initio calculations for the phonon dispersion are from Ref. Horzum et al., 2013. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012); Huang, Da, and Liang (2013); Sevik (2014); Kumar and Schwingenschlogl (2015); Huang, Zhang, and Zhang (2016) Fig. 55 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 115. The parameters for the three-body SW potential used by GULP are shown in Tab. 116. Parameters for the SW potential used by LAMMPS are listed in Tab. 117. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-MoSe2 using LAMMPS, because the angles around atom Mo in Fig. 1 (with M=Mo and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Mo and X=Se) shows that, for 1H-MoSe2, we can differentiate these angles around the Mo atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Mo atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-MoSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 56 shows the stress-strain curve during the tension of a single-layer 1H-MoSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-MoSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-MoSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 103.0 N/m and 101.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in considerable agreement with the experimental results, eg. 103.9 N/m from Refs Cakir, Peeters, and Sevik, 2014, or 113.9 N/m from Ref. Li, Medhekar, and Shenoy, 2013. The Poisson’s ratio from the VFF model and the SW potential is , which agrees quite well with the ab initio value of 0.23.Cakir, Peeters, and Sevik (2014)
We have determined the nonlinear parameter to be in Eq. (5) by fitting to the third-order nonlinear elastic constant from the ab initio calculations.Li, Medhekar, and Shenoy (2013) We have extracted the value of N/m by fitting the stress-strain relation along the armchair direction in the ab initio calculations to the function with as the Young’s modulus. The values of from the present SW potential are -365.4 N/m and -402.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 13.6 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 13.0 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
XXX 1H-MoTe2
Most existing theoretical studies on the single-layer 1H-MoTe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-MoTe2.
The structure for the single-layer 1H-MoTe2 is shown in Fig. 1 (with M=Mo and X=Te). Each Mo atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Mo atoms. The structural parameters are from Ref. Guo et al., 2015, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 118 shows four VFF terms for the 1H-MoTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 57 (a). The ab initio calculations for the phonon dispersion are from Ref. Guo et al., 2015. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012); Kan et al. (2015); Huang, Zhang, and Zhang (2016) Fig. 57 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 119. The parameters for the three-body SW potential used by GULP are shown in Tab. 120. Parameters for the SW potential used by LAMMPS are listed in Tab. 121. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-MoTe2 using LAMMPS, because the angles around atom Mo in Fig. 1 (with M=Mo and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Mo and X=Te) shows that, for 1H-MoTe2, we can differentiate these angles around the Mo atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Mo atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-MoTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 58 shows the stress-strain curve for the tension of a single-layer 1H-MoTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-MoTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-MoTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 79.8 N/m and 78.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in considerable agreement with the experimental results, eg. 79.4 N/m from Refs Cakir, Peeters, and Sevik, 2014, or 87.0 N/m from Ref. Li, Medhekar, and Shenoy, 2013. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.24.Cakir, Peeters, and Sevik (2014)
We have determined the nonlinear parameter to be in Eq. (5) by fitting to the third-order nonlinear elastic constant from the ab initio calculations.Li, Medhekar, and Shenoy (2013) We have extracted the value of N/m by fitting the stress-strain relation along the armchair direction in the ab initio calculations to the function with as the Young’s modulus. The values of from the present SW potential are -250.5 N/m and -276.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.7 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.1 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XXXI 1H-TaS2
In 1983, the VFF model was developed to investigate the lattice dynamical properties in the bulk 2H-TaS2.FlcMullan (1983) In this section, we will develop the SW potential for the single-layer 1H-TaS2.
The structure for the single-layer 1H-TaS2 is shown in Fig. 1 (with M=Ta and X=S). Each Ta atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Ta atoms. The structural parameters are from Ref. FlcMullan, 1983, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 122 shows the VFF terms for the 1H-TaS2, one of which is the bond stretching interaction shown by Eq. (1) while the others are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 59 (a). The theoretical phonon frequencies (gray pentagons) are from Ref. FlcMullan, 1983, which are the phonon dispersion of bulk 2H-TaS2. We have used these phonon frequencies as the phonon dispersion of the single-layer 1H-TaS2, as the inter-layer interaction in the bulk 2H-TaS2 only induces weak effects on the two inplane acoustic branches. The inter-layer coupling will strengthen the out-of-plane acoustic (flexural) branch, so the flexural branch from the present VFF model (blue line) is lower than the theoretical results for bulk 2H-TaS2 (gray pentagons). Fig. 59 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 123. The parameters for the three-body SW potential used by GULP are shown in Tab. 124. Parameters for the SW potential used by LAMMPS are listed in Tab. 125. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-TaS2 using LAMMPS, because the angles around atom Ta in Fig. 1 (with M=Ta and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ta and X=S) shows that, for 1H-TaS2, we can differentiate these angles around the Ta atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ta atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-TaS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 60 shows the stress-strain curve for the tension of a single-layer 1H-TaS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-TaS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-TaS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 87.4 N/m and 86.6 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-TaS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -313.0 N/m and -349.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.4 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
XXXII 1H-TaSe2
The VFF model was developed to investigate the lattice dynamical properties in the bulk 2H-TaSe2.Feldman (1982); FlcMullan (1983) In this section, we will develop the SW potential for the single-layer 1H-TaSe2.
The structure for the single-layer 1H-TaSe2 is shown in Fig. 1 (with M=Ta and X=Se). Each Ta atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Ta atoms. The structural parameters are from Ref. FlcMullan, 1983, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 126 shows the VFF terms for the 1H-TaSe2, one of which is the bond stretching interaction shown by Eq. (1) while the others are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 61 (a). The theoretical phonon frequencies (gray pentagons) are from Ref. FlcMullan, 1983, which are the phonon dispersion of bulk 2H-TaSe2. We have used these phonon frequencies as the phonon dispersion of the single-layer 1H-TaSe2, as the inter-layer interaction in the bulk 2H-TaSe2 only induces weak effects on the two in-plane acoustic branches. The inter-layer coupling will strengthen the out-of-plane acoustic branch (flexural branch), so the flexural branch from the present VFF model (blue line) is lower than the theoretical results for bulk 2H-TaSe2 (gray pentagons). Fig. 61 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 127. The parameters for the three-body SW potential used by GULP are shown in Tab. 128. Parameters for the SW potential used by LAMMPS are listed in Tab. 129. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-TaSe2 using LAMMPS, because the angles around atom Ta in Fig. 1 (with M=Ta and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=Ta and X=Se) shows that, for 1H-TaSe2, we can differentiate these angles around the Ta atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one Ta atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-TaSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 62 shows the stress-strain curve for the tension of a single-layer 1H-TaSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-TaSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-TaSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 80.8 N/m and 81.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for the nonlinear quantities in the single-layer 1H-TaSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -263.3 N/m and -308.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.3 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.7 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
XXXIII 1H-WO2
Most existing theoretical studies on the single-layer 1H-WO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1H-WO2.
The structure for the single-layer 1H-WO2 is shown in Fig. 1 (with M=W and X=O). Each W atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three W atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms O and O’ are from different (top or bottom) group.
Table 130 shows four VFF terms for the single-layer 1H-WO2, one of which is the bond stretching interaction shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 63 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 63 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 131. The parameters for the three-body SW potential used by GULP are shown in Tab. 132. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 133. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-WO2 using LAMMPS, because the angles around atom W in Fig. 1 (with M=W and X=O) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=W and X=O) shows that, for 1H-WO2, we can differentiate these angles around the W atom by assigning these six neighboring O atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one W atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-WO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 64 shows the stress-strain curve for the tension of a single-layer 1H-WO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-WO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-WO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 237.1 N/m and 237.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1H-WO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -1218.0 N/m and -1312.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 22.6 Nm*-1* at the ultimate strain of 0.18 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 21.8 Nm*-1* at the ultimate strain of 0.21 in the zigzag direction at the low temperature of 1 K.
XXXIV 1H-WS2
Most existing theoretical studies on the single-layer 1H-WS2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-WS2.
The structure for the single-layer 1H-WS2 is shown in Fig. 1 (with M=W and X=S). Each W atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three W atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms S and S’ are from different (top or bottom) group.
Table 134 shows the VFF terms for the 1H-WS2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 65 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Da, and Liang, 2013. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012); Molina-Sánchez and Wirtz (2011); Gu and Yang (2014); Huang et al. (2014); Huang, Zhang, and Zhang (2016) Fig. 65 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 135. The parameters for the three-body SW potential used by GULP are shown in Tab. 136. Parameters for the SW potential used by LAMMPS are listed in Tab. 137. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-WS2 using LAMMPS, because the angles around atom W in Fig. 1 (with M=W and X=S) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=W and X=S) shows that, for 1H-WS2, we can differentiate these angles around the W atom by assigning these six neighboring S atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one W atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-WS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 66 shows the stress-strain curve for the tension of a single-layer 1H-WS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-WS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-WS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 121.5 N/m along both armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 139.6 N/m from Ref. Cakir, Peeters, and Sevik, 2014, or 148.5 N/m from Ref. Li, Medhekar, and Shenoy, 2013. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.22.Cakir, Peeters, and Sevik (2014)
We have determined the nonlinear parameter to be in Eq. (5) by fitting to the third-order nonlinear elastic constant from the ab initio calculations.Li, Medhekar, and Shenoy (2013) We have extracted the value of N/m by fitting the stress-strain relation along the armchair direction in the ab initio calculations to the function with as the Young’s modulus. The values of from the present SW potential are -472.8 N/m and -529.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 14.7 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 14.1 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XXXV 1H-WSe2
Most existing theoretical studies on the single-layer 1H-WSe2 are based on the first-principles calculations. Norouzzadeh and Singh provided one set of parameters for the SW potential for the single-layer 1H-WSe2.Norouzzadeh and Singh (2017) In this section, we will develop both VFF model and the SW potential for the single-layer 1H-WSe2.
The structure for the single-layer 1H-WSe2 is shown in Fig. 1 (with M=W and X=Se). Each W atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three W atoms. The structural parameters are from Ref. Ataca, Sahin, and Ciraci, 2012, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Se and Se’ are from different (top or bottom) group.
Table 138 shows three VFF terms for the 1H-WSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 67 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Da, and Liang, 2013. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012); Huang et al. (2014); Zhou and Chen (2015); Kumar and Schwingenschlogl (2015); Huang, Zhang, and Zhang (2016) Fig. 67 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 139. The parameters for the three-body SW potential used by GULP are shown in Tab. 140. Parameters for the SW potential used by LAMMPS are listed in Tab. 141. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-WSe2 using LAMMPS, because the angles around atom W in Fig. 1 (with M=W and X=Se) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=W and X=Se) shows that, for 1H-WSe2, we can differentiate these angles around the W atom by assigning these six neighboring Se atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one W atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-WSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 68 shows the stress-strain curve for the tension of a single-layer 1H-WSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-WSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-WSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 124.1 N/m and 123.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 116.0 N/m from Ref. Cakir, Peeters, and Sevik, 2014, or 126.2 N/m from Ref. Li, Medhekar, and Shenoy, 2013. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.19.Cakir, Peeters, and Sevik (2014)
We have determined the nonlinear parameter to be in Eq. (5) by fitting to the third-order nonlinear elastic constant from the ab initio calculations.Li, Medhekar, and Shenoy (2013) We have extracted the value of N/m by fitting the stress-strain relation along the armchair direction in the ab initio calculations to the function with as the Young’s modulus. The values of from the present SW potential are -400.4 N/m and -444.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 17.8 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 17.1 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XXXVI 1H-WTe2
Most existing theoretical studies on the single-layer 1H-WTe2 are based on the first-principles calculations. In this section, we will develop both VFF model and the SW potential for the single-layer 1H-WTe2.
The bulk WTe2 has the trigonally coordinated H phase structure.Mar, Jobic, and Ibers (1992) However, it has been predicted that the structure of the single-layer WTe2 can be either the trigonally coordinated H phaseAtaca, Sahin, and Ciraci (2012) or the octahedrally coordinated phase,Dawson and Bullett (1987); Brown (1996); Jana et al. (2015); Jiang, Gao, and Wang (2016) with phase as the more stable structure.Torun et al. (2016) We will thus consider both phases in the present paper. This section is devoted to the H phase for the WTe2 (1H-WTe2), while the SW potential for the -WTe2 (1T-WTe2) is presented in another section.
The structure for the single-layer 1H-WTe2 is shown in Fig. 1 (with M=W and X=Te). Each W atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three W atoms. The structural parameters are from Ref. Torun et al., 2016, including the lattice constant Å, and the bond length Å. The resultant angles are and , in which atoms Te and Te’ are from different (top or bottom) group.
Table 142 shows the VFF terms for the 1H-WTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 69 (a). The ab initio calculations for the phonon dispersion are from Ref. Torun et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Ataca, Sahin, and Ciraci (2012) Fig. 69 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 143. The parameters for the three-body SW potential used by GULP are shown in Tab. 144. Parameters for the SW potential used by LAMMPS are listed in Tab. 145. We note that twelve atom types have been introduced for the simulation of the single-layer 1H-WTe2 using LAMMPS, because the angles around atom W in Fig. 1 (with M=W and X=Te) are not distinguishable in LAMMPS. We have suggested two options to differentiate these angles by implementing some additional constraints in LAMMPS, which can be accomplished by modifying the source file of LAMMPS.Jiang, Park, and Rabczuk (2013); Zhou and Jiang (2017) According to our experience, it is not so convenient for some users to implement these constraints and recompile the LAMMPS package. Hence, in the present work, we differentiate the angles by introducing more atom types, so it is not necessary to modify the LAMMPS package. Fig. 2 (with M=W and X=Te) shows that, for 1H-WTe2, we can differentiate these angles around the W atom by assigning these six neighboring Te atoms with different atom types. It can be found that twelve atom types are necessary for the purpose of differentiating all six neighbors around one W atom.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1H-WTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 70 shows the stress-strain curve for the tension of a single-layer 1H-WTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1H-WTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1H-WTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 82.7 N/m and 81.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are in reasonably agreement with the ab initio results, eg. 86.4 N/m from Ref. Cakir, Peeters, and Sevik, 2014, or 93.9 N/m from Ref. Li, Medhekar, and Shenoy, 2013. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio value of 0.18.Cakir, Peeters, and Sevik (2014)
We have determined the nonlinear parameter to be in Eq. (5) by fitting to the third-order nonlinear elastic constant from the ab initio calculations.Li, Medhekar, and Shenoy (2013) We have extracted the value of N/m by fitting the stress-strain relation along the armchair direction in the ab initio calculations to the function with as the Young’s modulus. The values of from the present SW potential are -269.4 N/m and -297.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.8 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.3 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XXXVII 1T-ScO2
Most existing theoretical studies on the single-layer 1T-ScO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ScO2.
The structure for the single-layer 1T-ScO2 is shown in Fig. 71 (with M=Sc and X=O). Each Ni atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with O atoms from the same (top or bottom) group, and .
Table 146 shows three VFF terms for the single-layer 1T-ScO2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both O atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 72 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 72 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 147. The parameters for the three-body SW potential used by GULP are shown in Tab. 148. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 149.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ScO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 73 shows the stress-strain curve for the tension of a single-layer 1T-ScO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ScO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ScO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 100.9 N/m and 100.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-ScO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -422.4 N/m and -453.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.7 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.3 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XXXVIII 1T-ScS2
Most existing theoretical studies on the single-layer 1T-ScS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ScS2.
The structure for the single-layer 1T-ScS2 is shown in Fig. 71 (with M=Sc and X=S). Each Sc atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angle is and with S atoms from the same (top or bottom) group.
Table 150 shows three VFF terms for the single-layer 1T-ScS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 74 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 74 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 151. The parameters for the three-body SW potential used by GULP are shown in Tab. 152. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 153.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ScS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 75 shows the stress-strain curve for the tension of a single-layer 1T-ScS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ScS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ScS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 30.0 N/m and 29.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-ScS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -113.7 N/m and -124.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 3.8 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.6 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
XXXIX 1T-ScSe2
Most existing theoretical studies on the single-layer 1T-ScSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ScSe2.
The structure for the single-layer 1T-ScSe2 is shown in Fig. 71 (with M=Sc and X=Se). Each Sc atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angle is and with Se atoms from the same (top or bottom) group.
Table 154 shows three VFF terms for the single-layer 1T-ScSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 76 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 76 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 155. The parameters for the three-body SW potential used by GULP are shown in Tab. 156. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 157.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ScSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 77 shows the stress-strain curve for the tension of a single-layer 1T-ScSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ScSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ScSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 36.4 N/m and 36.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-ScSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -113.7 N/m and -130.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.3 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XL 1T-ScTe2
Most existing theoretical studies on the single-layer 1T-ScTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ScTe2.
The structure for the single-layer 1T-ScTe2 is shown in Fig. 71 (with M=Sc and X=Te). Each Sc atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Sc atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å, and the bond length Å. The resultant angle is and with Se atoms from the same (top or bottom) group.
Table 158 shows three VFF terms for the single-layer 1T-ScTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 78 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 78 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 159. The parameters for the three-body SW potential used by GULP are shown in Tab. 160. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 161.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ScTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 79 shows the stress-strain curve for the tension of a single-layer 1T-ScTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ScTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ScTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 31.4 N/m and 31.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-ScTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -81.2 N/m and -96.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
XLI 1T-TiS2
Most existing theoretical studies on the single-layer 1T-TiS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TiS2.
The structure for the single-layer 1T-TiS2 is shown in Fig. 71 (with M=Ti and X=S). Each Ti atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Ti atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 162 shows three VFF terms for the single-layer 1T-TiS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 85 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 163. The parameters for the three-body SW potential used by GULP are shown in Tab. 164. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 165.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TiS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 80 shows the stress-strain curve for the tension of a single-layer 1T-TiS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TiS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TiS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 75.0 N/m and 74.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 85 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TiS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -220.8 N/m and -264.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.4 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 81 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
XLII 1T-TiSe2
Most existing theoretical studies on the single-layer 1T-TiSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TiSe2.
The structure for the single-layer 1T-TiSe2 is shown in Fig. 71 (with M=Ti and X=Se). Each Ti atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Ti atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Se atoms from the same (top or bottom) group, and .
Table 166 shows three VFF terms for the single-layer 1T-TiSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 70 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 167. The parameters for the three-body SW potential used by GULP are shown in Tab. 168. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 169.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TiSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 82 shows the stress-strain curve for the tension of a single-layer 1T-TiSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TiSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TiSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 59.2 N/m and 58.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 70 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TiSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -166.5 N/m and -201.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.7 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.3 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 83 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
XLIII 1T-TiTe2
Most existing theoretical studies on the single-layer 1T-TiTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TiTe2.
The structure for the single-layer 1T-TiTe2 is shown in Fig. 71 (with M=Ti and X=Te). Each Ti atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ti atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Te atoms from the same (top or bottom) group, and .
Table 170 shows three VFF terms for the single-layer 1T-TiTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 46 N/m and the Poisson’s ratio as 0.15.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 171. The parameters for the three-body SW potential used by GULP are shown in Tab. 172. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 173.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TiTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 84 shows the stress-strain curve for the tension of a single-layer 1T-TiTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TiTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TiTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 41.4 N/m and 41.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 46 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TiTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -161.3 N/m and -181.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.7 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
Fig. 85 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
XLIV 1T-VS2
Most existing theoretical studies on the single-layer 1T-VS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-VS2.
The structure for the single-layer 1T-VS2 is shown in Fig. 71 (with M=V and X=S). Each V atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three V atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 174 shows three VFF terms for the single-layer 1T-VS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 86 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. The lowest acoustic branch (flexural mode) is linear and very close to the inplane transverse acoustic branch in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 86 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 175. The parameters for the three-body SW potential used by GULP are shown in Tab. 176. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 177.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-VS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 87 shows the stress-strain curve for the tension of a single-layer 1T-VS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-VS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-VS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 87.1 N/m and 86.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-VS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -230.5 N/m and -283.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 13.3 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.7 Nm*-1* at the ultimate strain of 0.30 in the zigzag direction at the low temperature of 1 K.
XLV 1T-VSe2
Most existing theoretical studies on the single-layer 1T-VSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-VSe2.
The structure for the single-layer 1T-VSe2 is shown in Fig. 71 (with M=V and X=Se). Each V atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three V atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Se atoms from the same (top or bottom) group, and .
Table 178 shows three VFF terms for the single-layer 1T-VSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 88 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 88 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 179. The parameters for the three-body SW potential used by GULP are shown in Tab. 180. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 181.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-VSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 89 shows the stress-strain curve for the tension of a single-layer 1T-VSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-VSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-VSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 78.4 N/m and 78.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-VSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -168.5 N/m and -218.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 13.1 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.5 Nm*-1* at the ultimate strain of 0.32 in the zigzag direction at the low temperature of 1 K.
XLVI 1T-VTe2
Most existing theoretical studies on the single-layer 1T-VTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-VTe2.
The structure for the single-layer 1T-VTe2 is shown in Fig. 71 (with M=V and X=Te). Each V atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three V atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Te atoms from the same (top or bottom) group, and .
Table 182 shows three VFF terms for the single-layer 1T-VTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 67 N/m and the Poisson’s ratio as 0.24.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 183. The parameters for the three-body SW potential used by GULP are shown in Tab. 184. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 185.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-VTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 90 shows the stress-strain curve for the tension of a single-layer 1T-VTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-VTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-VTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 61.2 N/m and 61.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 67 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-VTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -95.8 N/m and -135.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.5 Nm*-1* at the ultimate strain of 0.30 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.0 Nm*-1* at the ultimate strain of 0.34 in the zigzag direction at the low temperature of 1 K.
Fig. 91 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
XLVII 1T-MnO2
Most existing theoretical studies on the single-layer 1T-MnO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MnO2.
The structure for the single-layer 1T-MnO2 is shown in Fig. 71 (with M=Mn and X=O). Each Mn atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Mn atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with O atoms from the same (top or bottom) group, and .
Table 186 shows three VFF terms for the single-layer 1T-MnO2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both O atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 92 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 92 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 187. The parameters for the three-body SW potential used by GULP are shown in Tab. 188. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 189.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MnO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 93 shows the stress-strain curve for the tension of a single-layer 1T-MnO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MnO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MnO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 156.3 N/m and 155.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-MnO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -711.7 N/m and -756.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 16.8 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 16.2 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
XLVIII 1T-MnS2
Most existing theoretical studies on the single-layer 1T-MnS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MnS2.
The structure for the single-layer 1T-MnS2 is shown in Fig. 71 (with M=Mn and X=S). Each Mn atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Mn atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 190 shows three VFF terms for the single-layer 1T-MnS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 94 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 94 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 191. The parameters for the three-body SW potential used by GULP are shown in Tab. 192. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 193.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MnS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 95 shows the stress-strain curve for the tension of a single-layer 1T-MnS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MnS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MnS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 47.1 N/m and 46.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-MnS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -193.8 N/m and -210.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.5 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.3 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XLIX 1T-MnSe2
Most existing theoretical studies on the single-layer 1T-MnSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MnSe2.
The structure for the single-layer 1T-MnSe2 is shown in Fig. 71 (with M=Mn and X=Se). Each Mn atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Mn atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Se atoms from the same (top or bottom) group, and .
Table 194 shows three VFF terms for the single-layer 1T-MnSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 96 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 96 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 195. The parameters for the three-body SW potential used by GULP are shown in Tab. 196. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 197.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MnSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 97 shows the stress-strain curve for the tension of a single-layer 1T-MnSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MnSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MnSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 43.2 N/m and 42.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-MnSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -163.4 N/m and -179.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.4 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
L 1T-MnTe2
Most existing theoretical studies on the single-layer 1T-MnTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MnTe2.
The structure for the single-layer 1T-MnTe2 is shown in Fig. 71 (with M=Mn and X=Te). Each Mn atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Mn atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Te atoms from the same (top or bottom) group, and .
Table 198 shows three VFF terms for the single-layer 1T-MnTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 98 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 98 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 199. The parameters for the three-body SW potential used by GULP are shown in Tab. 200. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 201.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MnTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 99 shows the stress-strain curve for the tension of a single-layer 1T-MnTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MnTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MnTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 38.5 N/m and 38.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-MnTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -133.5 N/m and -149.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
LI 1T-CoTe2
Most existing theoretical studies on the single-layer 1T-CoTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-CoTe2.
The structure for the single-layer 1T-CoTe2 is shown in Fig. 71 (with M=Co and X=Te). Each Co atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Co atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 202 shows three VFF terms for the single-layer 1T-CoTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 59 N/m and the Poisson’s ratio as 0.14.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 203. The parameters for the three-body SW potential used by GULP are shown in Tab. 204. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 205.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-CoTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 100 shows the stress-strain curve for the tension of a single-layer 1T-CoTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-CoTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-CoTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 50.5 N/m and 50.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 59 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-CoTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -221.5 N/m and -238.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.6 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.4 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
Fig. 101 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LII 1T-NiO2
Most existing theoretical studies on the single-layer 1T-NiO2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NiO2.
The structure for the single-layer 1T-NiO2 is shown in Fig. 71 (with M=Ni and X=O). Each Ni atom is surrounded by six O atoms. These O atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each O atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with O atoms from the same (top or bottom) group, and .
Table 206 shows three VFF terms for the single-layer 1T-NiO2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both O atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 102 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 102 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 207. The parameters for the three-body SW potential used by GULP are shown in Tab. 208. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 209.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NiO2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 103 shows the stress-strain curve for the tension of a single-layer 1T-NiO2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NiO2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NiO2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 163.3 N/m and 162.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-NiO2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -748.7 N/m and -796.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 17.4 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 16.8 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
LIII 1T-NiS2
Most existing theoretical studies on the single-layer 1T-NiS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NiS2.
The structure for the single-layer 1T-NiS2 is shown in Fig. 71 (with M=Ni and X=S). Each Ni atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 210 shows three VFF terms for the single-layer 1T-NiS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 104 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 104 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 211. The parameters for the three-body SW potential used by GULP are shown in Tab. 212. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 213.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NiS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 105 shows the stress-strain curve for the tension of a single-layer 1T-NiS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NiS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NiS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 74.2 N/m and 73.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-NiS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -274.5 N/m and -301.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.5 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.2 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
LIV 1T-NiSe2
Most existing theoretical studies on the single-layer 1T-NiSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NiSe2.
The structure for the single-layer 1T-NiSe2 is shown in Fig. 71 (with M=Ni and X=Se). Each Ni atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 214 shows three VFF terms for the single-layer 1T-NiSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the two in-plane acoustic branches in the phonon dispersion along the M as shown in Fig. 106 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. Fig. 106 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 215. The parameters for the three-body SW potential used by GULP are shown in Tab. 216. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 217.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NiSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 107 shows the stress-strain curve for the tension of a single-layer 1T-NiSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NiSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NiSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 70.9 N/m and 70.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-NiSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -263.7 N/m and -289.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.7 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
LV 1T-NiTe2
Most existing theoretical studies on the single-layer 1T-NiTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NiTe2.
The structure for the single-layer 1T-NiTe2 is shown in Fig. 71 (with M=Ni and X=Te). Each Ni atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ni atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 218 shows three VFF terms for the single-layer 1T-NiTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 44 N/m and the Poisson’s ratio as 0.14.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 219. The parameters for the three-body SW potential used by GULP are shown in Tab. 220. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 221.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NiTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 108 shows the stress-strain curve for the tension of a single-layer 1T-NiTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NiTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NiTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 42.6 N/m and 42.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-NiTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -187.6 N/m and -200.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.7 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.6 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
Fig. 109 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LVI 1T-ZrS2
Most existing theoretical studies on the single-layer 1T-ZrS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ZrS2.
The structure for the single-layer 1T-ZrS2 is shown in Fig. 71 (with M=Zr and X=S). Each Zr atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Zr atoms. The structural parameters are from the first-principles calculations,Li, Kang, and Li (2014) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 222 shows three VFF terms for the single-layer 1T-ZrS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 110 (a). The ab initio calculations for the phonon dispersion are from Ref. Gu and Yang, 2014. Similar phonon dispersion can also be found in other ab initio calculations.Huang, Zhang, and Zhang (2016) Fig. 110 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 223. The parameters for the three-body SW potential used by GULP are shown in Tab. 224. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 225.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ZrS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 111 shows the stress-strain curve for the tension of a single-layer 1T-ZrS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ZrS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ZrS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 71.8 N/m and 71.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are close to the ab initio results at 0 K temperature, eg. 75.74 Nm*-1* in Ref. Li, Kang, and Li, 2014. The Poisson’s ratio from the VFF model and the SW potential is , which are comparable with the ab initio resultLi, Kang, and Li (2014) of 0.22.
There is no available value for nonlinear quantities in the single-layer 1T-ZrS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -268.9 N/m and -305.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.9 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.5 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
LVII 1T-ZrSe2
Most existing theoretical studies on the single-layer 1T-ZrSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ZrSe2.
The structure for the single-layer 1T-ZrSe2 is shown in Fig. 71 (with M=Zr and X=Se). Each Zr atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Zr atoms. The structural parameters are from the first-principles calculations,Zhang et al. (2014a) including the lattice constant Å, and the position of the Se atom with respective to the Zr atomic plane Å. The resultant angles are with Se atoms from the same (top or bottom) group, and .
Table 226 shows three VFF terms for the single-layer 1T-ZrSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 112 (a). The ab initio calculations for the phonon dispersion are from Ref. Ding et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Huang, Zhang, and Zhang (2016) Fig. 112 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 227. The parameters for the three-body SW potential used by GULP are shown in Tab. 228. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 229.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ZrSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 113 shows the stress-strain curve for the tension of a single-layer 1T-ZrSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ZrSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ZrSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 66.7 N/m and 66.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-ZrSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -219.6 N/m and -256.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
LVIII 1T-ZrTe2
Most existing theoretical studies on the single-layer 1T-ZrTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ZrTe2.
The structure for the single-layer 1T-ZrTe2 is shown in Fig. 71 (with M=Zr and X=Te). Each Zr atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Zr atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 230 shows three VFF terms for the single-layer 1T-ZrTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 44 N/m and the Poisson’s ratio as 0.13.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 231. The parameters for the three-body SW potential used by GULP are shown in Tab. 232. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 233.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ZrTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 114 shows the stress-strain curve for the tension of a single-layer 1T-ZrTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ZrTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ZrTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 39.2 N/m and 39.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 44 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-ZrTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -187.2 N/m and -201.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.0 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.9 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
Fig. 115 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LIX 1T-NbS2
Most existing theoretical studies on the single-layer 1T-NbS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NbS2.
The structure for the single-layer 1T-NbS2 is shown in Fig. 71 (with M=Nb and X=S). Each Nb atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Nb atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 234 shows three VFF terms for the single-layer 1T-NbS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 116 (a). The ab initio calculations for the phonon dispersion are from Ref. Ataca, Sahin, and Ciraci, 2012. The lowest acoustic branch (flexural mode) is linear and very close to the inplane transverse acoustic branch in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 116 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 235. The parameters for the three-body SW potential used by GULP are shown in Tab. 236. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 237.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NbS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 117 shows the stress-strain curve for the tension of a single-layer 1T-NbS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NbS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NbS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 73.8 N/m and 73.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-NbS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -250.5 N/m and -290.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.7 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.4 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
LX 1T-NbSe2
Most existing theoretical studies on the single-layer 1T-NbSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NbSe2.
The structure for the single-layer 1T-NbSe2 is shown in Fig. 71 (with M=Nb and X=Se). Each Nb atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Nb atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Se atoms from the same (top or bottom) group, and .
Table 238 shows three VFF terms for the single-layer 1T-NbSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 73 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 239. The parameters for the three-body SW potential used by GULP are shown in Tab. 240. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 241.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NbSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 118 shows the stress-strain curve for the tension of a single-layer 1T-NbSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NbSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NbSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 67.1 N/m and 66.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 73 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically lead to about 10% underestimation for the Young’s modulus value.
There is no available value for nonlinear quantities in the single-layer 1T-NbSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -193.5 N/m and -233.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.7 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.3 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 119 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXI 1T-NbTe2
Most existing theoretical studies on the single-layer 1T-NbTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-NbTe2.
The structure for the single-layer 1T-NbTe2 is shown in Fig. 71 (with M=Nb and X=Te). Each Nb atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Nb atoms. The structural parameters are from the first-principles calculations,Ataca, Sahin, and Ciraci (2012) including the lattice constant Å and the bond length Å. The resultant angles are with Te atoms from the same (top or bottom) group, and .
Table 242 shows three VFF terms for the single-layer 1T-NbTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 56 N/m and the Poisson’s ratio as 0.11.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 243. The parameters for the three-body SW potential used by GULP are shown in Tab. 244. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 245.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-NbTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 120 shows the stress-strain curve for the tension of a single-layer 1T-NbTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-NbTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-NbTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 52.2 N/m and 51.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 56 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-NbTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -237.7 N/m and -265.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.4 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
Fig. 121 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXII 1T-MoS2
Most existing theoretical studies on the single-layer 1T-MoS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MoS2.
The structure for the single-layer 1T-MoS2 is shown in Fig. 71 (with M=Mo and X=S). Each Mo atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Mo atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 246 shows three VFF terms for the single-layer 1T-MoS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 103 N/m and the Poisson’s ratio as -0.07.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-MoS2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 247. The parameters for the three-body SW potential used by GULP are shown in Tab. 248. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 249.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MoS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 122 shows the stress-strain curve for the tension of a single-layer 1T-MoS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MoS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MoS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 88.7 N/m and 88.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 103 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-MoS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -595.2 N/m and -624.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.5 Nm*-1* at the ultimate strain of 0.14 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.5 Nm*-1* at the ultimate strain of 0.16 in the zigzag direction at the low temperature of 1 K.
Fig. 123 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXIII 1T-MoSe2
Most existing theoretical studies on the single-layer 1T-MoSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MoSe2.
The structure for the single-layer 1T-MoSe2 is shown in Fig. 71 (with M=Mo and X=Se). Each Mo atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Mo atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 250 shows three VFF terms for the single-layer 1T-MoSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 104 N/m and the Poisson’s ratio as -0.13.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-MoSe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 251. The parameters for the three-body SW potential used by GULP are shown in Tab. 252. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 253.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MoSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 124 shows the stress-strain curve for the tension of a single-layer 1T-MoSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MoSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MoSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 88.2 N/m and 87.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 104 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-MoSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -632.6 N/m and -629.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.13 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.2 Nm*-1* at the ultimate strain of 0.15 in the zigzag direction at the low temperature of 1 K.
Fig. 125 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXIV 1T-MoTe2
Most existing theoretical studies on the single-layer 1T-MoTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-MoTe2.
The structure for the single-layer 1T-MoTe2 is shown in Fig. 71 (with M=Mo and X=Te). Each Mo atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Mo atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 254 shows three VFF terms for the single-layer 1T-MoTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 92 N/m and the Poisson’s ratio as -0.07.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-MoTe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 255. The parameters for the three-body SW potential used by GULP are shown in Tab. 256. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 257.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-MoTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 126 shows the stress-strain curve for the tension of a single-layer 1T-MoTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-MoTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-MoTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 81.6 N/m and 81.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 92 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-MoTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -543.1 N/m and -558.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.0 Nm*-1* at the ultimate strain of 0.14 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.0 Nm*-1* at the ultimate strain of 0.16 in the zigzag direction at the low temperature of 1 K.
Fig. 127 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXV 1T-TcS2
Most existing theoretical studies on the single-layer 1T-TcS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TcS2.
The structure for the single-layer 1T-TcS2 is shown in Fig. 71 (with M=Tc and X=S). Each Tc atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Tc atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 258 shows three VFF terms for the single-layer 1T-TcS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 94 N/m and the Poisson’s ratio as -0.10.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-TcS2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 259. The parameters for the three-body SW potential used by GULP are shown in Tab. 260. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 261.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TcS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 128 shows the stress-strain curve for the tension of a single-layer 1T-TcS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TcS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TcS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 84.3 N/m and 84.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 94 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TcS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -572.0 N/m and -588.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.0 Nm*-1* at the ultimate strain of 0.13 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.16 in the zigzag direction at the low temperature of 1 K.
Fig. 129 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXVI 1T-TcSe2
Most existing theoretical studies on the single-layer 1T-TcSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TcSe2.
The structure for the single-layer 1T-TcSe2 is shown in Fig. 71 (with M=Tc and X=Se). Each Tc atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Tc atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 262 shows three VFF terms for the single-layer 1T-TcSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 104 N/m and the Poisson’s ratio as -0.04.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-TcSe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 263. The parameters for the three-body SW potential used by GULP are shown in Tab. 264. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 265.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TcSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 130 shows the stress-strain curve for the tension of a single-layer 1T-TcSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TcSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TcSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 88.8 N/m and 88.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 104 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TcSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -565.7 N/m and -587.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.8 Nm*-1* at the ultimate strain of 0.14 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.8 Nm*-1* at the ultimate strain of 0.17 in the zigzag direction at the low temperature of 1 K.
Fig. 131 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXVII 1T-TcTe2
Most existing theoretical studies on the single-layer 1T-TcTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TcTe2.
The structure for the single-layer 1T-TcTe2 is shown in Fig. 71 (with M=Tc and X=Te). Each Tc atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Tc atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 266 shows three VFF terms for the single-layer 1T-TcTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 34 N/m and the Poisson’s ratio as -0.36.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-TcTe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 267. The parameters for the three-body SW potential used by GULP are shown in Tab. 268. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 269.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TcTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 132 shows the stress-strain curve for the tension of a single-layer 1T-TcTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TcTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TcTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 28.6 N/m along the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 34 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TcTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -207.8 N/m and -208.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 1.9 Nm*-1* at the ultimate strain of 0.11 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 2.0 Nm*-1* at the ultimate strain of 0.14 in the zigzag direction at the low temperature of 1 K. The ultimate strain decreases to be about 0.01 at 300 K, so the single-layer 1T-TcTe2 is not very stable at higher temperature. It is because this material is very soft and the Poisson’s ratio is very small (negative value).
Fig. 133 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXVIII 1T-RhTe2
Most existing theoretical studies on the single-layer 1T-RhTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-RhTe2.
The structure for the single-layer 1T-RhTe2 is shown in Fig. 71 (with M=Rh and X=Te). Each Rh atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Rh atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 270 shows three VFF terms for the single-layer 1T-RhTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 37 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 271. The parameters for the three-body SW potential used by GULP are shown in Tab. 272. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 273.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-RhTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 134 shows the stress-strain curve for the tension of a single-layer 1T-RhTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-RhTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-RhTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 32.1 N/m and 32.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 37 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-RhTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -103.1 N/m and -116.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.6 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.4 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 135 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXIX 1T-PdS2
Most existing theoretical studies on the single-layer 1T-PdS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PdS2.
The structure for the single-layer 1T-PdS2 is shown in Fig. 71 (with M=Pd and X=S). Each Pd atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Pd atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 274 shows three VFF terms for the single-layer 1T-PdS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 77 N/m and the Poisson’s ratio as 0.53.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 275. The parameters for the three-body SW potential used by GULP are shown in Tab. 276. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 277.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PdS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 136 shows the stress-strain curve for the tension of a single-layer 1T-PdS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PdS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PdS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 69.9 N/m and 69.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 77 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-PdS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -222.0 N/m and -248.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.1 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.7 Nm*-1* at the ultimate strain of 0.30 in the zigzag direction at the low temperature of 1 K.
Fig. 137 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXX 1T-PdSe2
Most existing theoretical studies on the single-layer 1T-PdSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PdSe2.
The structure for the single-layer 1T-PdSe2 is shown in Fig. 71 (with M=Pd and X=Se). Each Pd atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Pd atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 278 shows three VFF terms for the single-layer 1T-PdSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 66 N/m and the Poisson’s ratio as 0.45.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 279. The parameters for the three-body SW potential used by GULP are shown in Tab. 280. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 281.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PdSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 138 shows the stress-strain curve for the tension of a single-layer 1T-PdSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PdSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PdSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 65.5 N/m and 65.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-PdSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -194.7 N/m and -222.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.9 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.5 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
Fig. 139 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXI 1T-PdTe2
Most existing theoretical studies on the single-layer 1T-PdTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PdTe2.
The structure for the single-layer 1T-PdTe2 is shown in Fig. 71 (with M=Pd and X=Te). Each Pd atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Pd atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 282 shows three VFF terms for the single-layer 1T-PdTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 63 N/m and the Poisson’s ratio as 0.35.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 283. The parameters for the three-body SW potential used by GULP are shown in Tab. 284. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 285.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PdTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 140 shows the stress-strain curve for the tension of a single-layer 1T-PdTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PdTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PdTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 61.6 N/m and 61.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-PdTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -178.8 N/m and -203.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.6 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.2 Nm*-1* at the ultimate strain of 0.32 in the zigzag direction at the low temperature of 1 K.
Fig. 141 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXII 1T-SnS2
Most existing theoretical studies on the single-layer 1T-SnS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-SnS2.
The structure for the single-layer 1T-SnS2 is shown in Fig. 71 (with M=Sn and X=S). Each Sn atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Sn atoms. The structural parameters are from the first-principles calculations,Huang, Zhang, and Zhang (2016) including the lattice constant Å, and the bond length Å. The resultant angles are , and with S atoms from the same (top or bottom) group.
Table 286 shows three VFF terms for the single-layer 1T-SnS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 142 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Zhang, and Zhang, 2016. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 142 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 287. The parameters for the three-body SW potential used by GULP are shown in Tab. 288. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 289.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-SnS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 143 shows the stress-strain curve for the tension of a single-layer 1T-SnS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-SnS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-SnS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 88.4 N/m and 87.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-SnS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -392.8 N/m and -421.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.6 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.3 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
LXXIII 1T-SnSe2
Most existing theoretical studies on the single-layer 1T-SnSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-SnSe2.
The structure for the single-layer 1T-SnSe2 is shown in Fig. 71 (with M=Sn and X=Se). Each Sn atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Sn atoms. The structural parameters are from the first-principles calculations,Huang, Zhang, and Zhang (2016) including the lattice constant Å, and the bond length Å. The resultant angles are , and with Se atoms from the same (top or bottom) group.
Table 290 shows three VFF terms for the single-layer 1T-SnSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 144 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Zhang, and Zhang, 2016. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 144 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 291. The parameters for the three-body SW potential used by GULP are shown in Tab. 292. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 293.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-SnSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 145 shows the stress-strain curve for the tension of a single-layer 1T-SnSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-SnSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-SnSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 82.0 N/m and 81.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-SnSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -339.2 N/m and -368.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.5 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.1 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
LXXIV 1T-HfS2
Most existing theoretical studies on the single-layer 1T-HfS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-HfS2.
The structure for the single-layer 1T-HfS2 is shown in Fig. 71 (with M=Hf and X=S). Each Hf atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Hf atoms. The structural parameters are from the first-principles calculations,Kang, Sahin, and Peeters (2015) including the lattice constant Å and the bond length Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 294 shows three VFF terms for the single-layer 1T-HfS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 146 (a). The ab initio calculations for the phonon dispersion are from Ref. Gu and Yang, 2014. Similar phonon dispersion can also be found in other ab initio calculations.Chen (2016); Huang, Zhang, and Zhang (2016) Fig. 146 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 295. The parameters for the three-body SW potential used by GULP are shown in Tab. 296. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 297.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-HfS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 147 shows the stress-strain curve for the tension of a single-layer 1T-HfS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-HfS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-HfS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 73.3 N/m and 72.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values are close to the ab initio results at 0 K temperature, eg. 79.86 Nm*-1* in Ref. Kang, Sahin, and Peeters, 2015. The Poisson’s ratio from the VFF model and the SW potential is , which agrees reasonably with the ab initio resultKang, Sahin, and Peeters (2015) of 0.19.
There is no available value for nonlinear quantities in the single-layer 1T-HfS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -280.9 N/m and -317.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.9 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
LXXV 1T-HfSe2
Most existing theoretical studies on the single-layer 1T-HfSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-HfSe2.
The structure for the single-layer 1T-HfSe2 is shown in Fig. 71 (with M=Hf and X=Se). Each Hf atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Hf atoms. The structural parameters are from the first-principles calculations,Zhang et al. (2014a) including the lattice constant Å, and the position of the Se atom with respective to the Hf atomic plane Å. The resultant angles are with S atoms from the same (top or bottom) group, and .
Table 298 shows three VFF terms for the single-layer 1T-HfSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 148 (a). The ab initio calculations for the phonon dispersion are from Ref. Ding et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Huang, Zhang, and Zhang (2016) Fig. 148 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 299. The parameters for the three-body SW potential used by GULP are shown in Tab. 300. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 301.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-HfSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 149 shows the stress-strain curve for the tension of a single-layer 1T-HfSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-HfSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-HfSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 67.3 N/m and 67.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-HfSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -221.5 N/m and -258.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.0 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.7 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
LXXVI 1T-HfTe2
Most existing theoretical studies on the single-layer 1T-HfTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-HfTe2.
The structure for the single-layer 1T-HfTe2 is shown in Fig. 71 (with M=Hf and X=Te). Each Hf atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Hf atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 302 shows three VFF terms for the single-layer 1T-HfTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 50 N/m and the Poisson’s ratio as 0.10.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 303. The parameters for the three-body SW potential used by GULP are shown in Tab. 304. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 305.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-HfTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 150 shows the stress-strain curve for the tension of a single-layer 1T-HfTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-HfTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-HfTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 43.1 N/m along the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 50 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-HfTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -204.3 N/m and -220.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.4 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.3 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
Fig. 151 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXVII 1T-TaS2
Most existing theoretical studies on the single-layer 1T-TaS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TaS2.
The structure for the single-layer 1T-TaS2 is shown in Fig. 71 (with M=Ta and X=S). Each Ta atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Ta atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 306 shows three VFF terms for the single-layer 1T-TaS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 101 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 307. The parameters for the three-body SW potential used by GULP are shown in Tab. 308. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 309.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TaS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 152 shows the stress-strain curve for the tension of a single-layer 1T-TaS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TaS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TaS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 87.8 N/m and 87.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 101 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TaS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -276.3 N/m and -313.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.7 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.2 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 153 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXVIII 1T-TaSe2
Most existing theoretical studies on the single-layer 1T-TaSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TaSe2.
The structure for the single-layer 1T-TaSe2 is shown in Fig. 71 (with M=Ta and X=Se). Each Ta atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Ta atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 310 shows three VFF terms for the single-layer 1T-TaSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 85 N/m and the Poisson’s ratio as 0.20.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 311. The parameters for the three-body SW potential used by GULP are shown in Tab. 312. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 313.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TaSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 154 shows the stress-strain curve for the tension of a single-layer 1T-TaSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TaSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TaSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 74.6 N/m and 74.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 85 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TaSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -231.7 N/m and -265.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.4 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 155 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXIX 1T-TaTe2
Most existing theoretical studies on the single-layer 1T-TaTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-TaTe2.
The structure for the single-layer 1T-TaTe2 is shown in Fig. 71 (with M=Ta and X=Te). Each Ta atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ta atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 314 shows three VFF terms for the single-layer 1T-TaTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 57 N/m and the Poisson’s ratio as 0.10.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 315. The parameters for the three-body SW potential used by GULP are shown in Tab. 316. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 317.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-TaTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 156 shows the stress-strain curve for the tension of a single-layer 1T-TaTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-TaTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-TaTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 50.3 N/m and 50.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 57 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-TaTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -247.1 N/m and -262.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
Fig. 157 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXX 1T-WS2
Most existing theoretical studies on the single-layer 1T-WS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-WS2.
The structure for the single-layer 1T-WS2 is shown in Fig. 71 (with M=W and X=S). Each W atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three W atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 318 shows three VFF terms for the single-layer 1T-WS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 113 N/m and the Poisson’s ratio as -0.03.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-WS2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 319. The parameters for the three-body SW potential used by GULP are shown in Tab. 320. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 321.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-WS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 158 shows the stress-strain curve for the tension of a single-layer 1T-WS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-WS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-WS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 100.2 N/m and 99.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 113 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-WS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -666.6 N/m and -660.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 7.7 Nm*-1* at the ultimate strain of 0.15 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.7 Nm*-1* at the ultimate strain of 0.17 in the zigzag direction at the low temperature of 1 K.
Fig. 159 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXI 1T-WSe2
Most existing theoretical studies on the single-layer 1T-WSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-WSe2.
The structure for the single-layer 1T-WSe2 is shown in Fig. 71 (with M=W and X=Se). Each W atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three W atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 322 shows three VFF terms for the single-layer 1T-WSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 94 N/m and the Poisson’s ratio as -0.15.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-WSe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 323. The parameters for the three-body SW potential used by GULP are shown in Tab. 324. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 325.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-WSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 160 shows the stress-strain curve for the tension of a single-layer 1T-WSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-WSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-WSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 80.5 N/m and 80.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 94 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-WSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -666.1 N/m and -580.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.5 Nm*-1* at the ultimate strain of 0.13 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.6 Nm*-1* at the ultimate strain of 0.15 in the zigzag direction at the low temperature of 1 K.
Fig. 161 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXII 1T-WTe2
Most existing theoretical studies on the single-layer 1T-WTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-WTe2.
The structure for the single-layer 1T-WTe2 is shown in Fig. 71 (with M=W and X=Te). Each W atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three W atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 326 shows three VFF terms for the single-layer 1T-WTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 88 N/m and the Poisson’s ratio as -0.18.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-WTe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 327. The parameters for the three-body SW potential used by GULP are shown in Tab. 328. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 329.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-WTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 162 shows the stress-strain curve for the tension of a single-layer 1T-WTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-WTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-WTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 75.9 N/m and 75.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 88 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-WTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -546.0 N/m and -551.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.1 Nm*-1* at the ultimate strain of 0.12 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.14 in the zigzag direction at the low temperature of 1 K.
Fig. 163 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXIII 1T-ReS2
Most existing theoretical studies on the single-layer 1T-ReS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ReS2.
The structure for the single-layer 1T-ReS2 is shown in Fig. 71 (with M=Re and X=S). Each Re atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Re atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 330 shows three VFF terms for the single-layer 1T-ReS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 90 N/m and the Poisson’s ratio as -0.11.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-ReS2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 331. The parameters for the three-body SW potential used by GULP are shown in Tab. 332. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 333.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ReS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 164 shows the stress-strain curve for the tension of a single-layer 1T-ReS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ReS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ReS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 78.1 N/m and 77.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 90 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-ReS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -537.1 N/m and -550.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.5 Nm*-1* at the ultimate strain of 0.13 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.6 Nm*-1* at the ultimate strain of 0.15 in the zigzag direction at the low temperature of 1 K.
Fig. 165 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXIV 1T-ReSe2
Most existing theoretical studies on the single-layer 1T-ReSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ReSe2.
The structure for the single-layer 1T-ReSe2 is shown in Fig. 71 (with M=Re and X=Se). Each Re atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Re atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 334 shows three VFF terms for the single-layer 1T-ReSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 123 N/m and the Poisson’s ratio as -0.03.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-ReSe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 335. The parameters for the three-body SW potential used by GULP are shown in Tab. 336. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 337.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ReSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 166 shows the stress-strain curve for the tension of a single-layer 1T-ReSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ReSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ReSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 108.2 N/m and 107.7 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 123 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-ReSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -669.3 N/m and -699.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.5 Nm*-1* at the ultimate strain of 0.14 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.4 Nm*-1* at the ultimate strain of 0.17 in the zigzag direction at the low temperature of 1 K.
Fig. 167 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXV 1T-ReTe2
Most existing theoretical studies on the single-layer 1T-ReTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-ReTe2.
The structure for the single-layer 1T-ReTe2 is shown in Fig. 71 (with M=Re and X=Te). Each Re atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Re atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 338 shows three VFF terms for the single-layer 1T-ReTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 71 N/m and the Poisson’s ratio as -0.22.Yu, Yan, and Ruzsinszky (2017) The ab initio calculations have predicted a negative Poisson’s ratio in the 1T-ReTe2, which was attributed to the orbital coupling in this material. The orbital coupling enhances the angle bending interaction in the VFF model. As a result, the value of the angle bending parameter is much larger than the bond stretching force constant parameter, which is typical in auxetic materials with negative Poisson’s ratio.Jiang et al. (2016)
The parameters for the two-body SW potential used by GULP are shown in Tab. 339. The parameters for the three-body SW potential used by GULP are shown in Tab. 340. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 341.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-ReTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 168 shows the stress-strain curve for the tension of a single-layer 1T-ReTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-ReTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-ReTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 59.4 N/m and 59.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 71 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-ReTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -416.1 N/m and -425.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.0 Nm*-1* at the ultimate strain of 0.12 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.1 Nm*-1* at the ultimate strain of 0.14 in the zigzag direction at the low temperature of 1 K.
Fig. 169 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXVI 1T-IrTe2
Most existing theoretical studies on the single-layer 1T-IrTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-IrTe2.
The structure for the single-layer 1T-IrTe2 is shown in Fig. 71 (with M=Ir and X=Te). Each Ir atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Ir atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 342 shows three VFF terms for the single-layer 1T-IrTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. We find that there are actually only two parameters in the VFF model, so we can determine their value by fitting to the Young’s modulus and the Poisson’s ratio of the system. The ab initio calculations have predicted the Young’s modulus to be 45 N/m and the Poisson’s ratio as 0.22.Yu, Yan, and Ruzsinszky (2017)
The parameters for the two-body SW potential used by GULP are shown in Tab. 343. The parameters for the three-body SW potential used by GULP are shown in Tab. 344. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 345.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-IrTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 170 shows the stress-strain curve for the tension of a single-layer 1T-IrTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-IrTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-IrTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 38.6 N/m and 38.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is . The fitted Young’s modulus value is about 10% smaller than the ab initio result of 45 N/m,Yu, Yan, and Ruzsinszky (2017) as only short-range interactions are considered in the present work. The long-range interactions are ignored, which typically leads to about 10% underestimation for the value of the Young’s modulus.
There is no available value for nonlinear quantities in the single-layer 1T-IrTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -127.7 N/m and -142.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.4 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
Fig. 171 shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
LXXXVII 1T-PtS2
Most existing theoretical studies on the single-layer 1T-PtS2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PtS2.
The structure for the single-layer 1T-PtS2 is shown in Fig. 71 (with M=Pt and X=S). Each Pt atom is surrounded by six S atoms. These S atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each S atom is connected to three Pt atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with S atoms from the same (top or bottom) group.
Table 346 shows three VFF terms for the single-layer 1T-PtS2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both S atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 172 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Zhang, and Zhang, 2016. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 172 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 347. The parameters for the three-body SW potential used by GULP are shown in Tab. 348. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 349.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PtS2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 173 shows the stress-strain curve for the tension of a single-layer 1T-PtS2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PtS2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PtS2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 105.9 N/m and 105.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-PtS2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -420.6 N/m and -457.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.8 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.3 Nm*-1* at the ultimate strain of 0.26 in the zigzag direction at the low temperature of 1 K.
LXXXVIII 1T-PtSe2
Most existing theoretical studies on the single-layer 1T-PtSe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PtSe2.
The structure for the single-layer 1T-PtSe2 is shown in Fig. 71 (with M=Pt and X=Se). Each Pt atom is surrounded by six Se atoms. These Se atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Se atom is connected to three Pt atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Se atoms from the same (top or bottom) group.
Table 350 shows three VFF terms for the single-layer 1T-PtSe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Se atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 174 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Zhang, and Zhang, 2016. The lowest acoustic branch (flexural mode) is almost linear in the ab initio calculations, which may due to the violation of the rigid rotational invariance.Jiang et al. (2015) Fig. 174 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 351. The parameters for the three-body SW potential used by GULP are shown in Tab. 352. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 353.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PtSe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 175 shows the stress-strain curve for the tension of a single-layer 1T-PtSe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PtSe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PtSe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 101.1 N/m and 100.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-PtSe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -391.4 N/m and -424.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.5 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 12.1 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
LXXXIX 1T-PtTe2
Most existing theoretical studies on the single-layer 1T-PtTe2 are based on the first-principles calculations. In this section, we will develop the SW potential for the single-layer 1T-PtTe2.
The structure for the single-layer 1T-PtTe2 is shown in Fig. 71 (with M=Pt and X=Te). Each Pt atom is surrounded by six Te atoms. These Te atoms are categorized into the top group (eg. atoms 1, 3, and 5) and bottom group (eg. atoms 2, 4, and 6). Each Te atom is connected to three Pt atoms. The structural parameters are from the first-principles calculations,Yu, Yan, and Ruzsinszky (2017) including the lattice constant Å, and the bond length Å, which is derived from the angle . The other angle is with Te atoms from the same (top or bottom) group.
Table 354 shows three VFF terms for the single-layer 1T-PtTe2, one of which is the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). We note that the angle bending term is for the angle with both Te atoms from the same (top or bottom) group. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 176 (a). The ab initio calculations for the phonon dispersion are from Ref. Huang, Zhang, and Zhang, 2016. Fig. 176 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 355. The parameters for the three-body SW potential used by GULP are shown in Tab. 356. Some representative parameters for the SW potential used by LAMMPS are listed in Tab. 357.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer 1T-PtTe2 under uniaxial tension at 1.0 K and 300.0 K. Fig. 177 shows the stress-strain curve for the tension of a single-layer 1T-PtTe2 of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer 1T-PtTe2 is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer 1T-PtTe2. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 89.1 N/m and 88.7 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer 1T-PtTe2. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -306.8 N/m and -340.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 12.1 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.6 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
XC Black phosphorus
The black phosphorus is also named the phosphorus. There are several empirical potentials available for the atomic interaction in the black phosphorus. A VFF model was proposed for the single-layer black phosphorus in 1982.Kaneta, Katayama-Yoshida, and Morita (1982) One of the present author (J.W.J.) simplified this VFF model by ignoring some angle-angle crossing terms, and use the simplified VFF model to develop the SW potential for the black phosphorus.Jiang (2015a) However, the mechanical properties from this SW potential are smaller than first-principles calculations, as some angle-angle crossing VFF terms can not be implemented in the SW potential. We will thus propose a new set of SW potential for the single-layer black phosphorus in this section.
The structure of the single-layer black phosphorus is shown in Fig. 178, with structural parameters from the ab initio calculations.Du et al. (2010) The black phosphorus has a puckered configuration as shown in Fig. 178 (b), where the pucker is perpendicular to the x-direction. The bases for the rectangular unit cell are Å and Å. For bulk black phosphorus, the basis lattice vector in the third direction is Å. There are four phosphorus atoms in the basic unit cell, and their relative coordinates are , , , and with and . Atoms are categorized into the top and bottom groups. Atoms in the top group are denoted by P1, while atoms in the bottom group are denoted by P2.
Table 358 shows four VFF terms for the single-layer black phosphorus, two of which are the bond stretching interactions shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). The force constant parameters are reasonably chosen to be the same for the two bond stretching terms denoted by and , as these two bonds have very close bond length value. The force constant parameters are the same for the two angle bending terms and , which have very similar chemical environment. These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the X as shown in Fig. 179 (a). The ab initio calculations for the phonon dispersion are from Ref. Zhu and Tomanek, 2014. Similar phonon dispersion can also be found in other ab initio calculations.Qin et al. (2014); Elahi et al. (2014); Ong et al. (2014); Aierken et al. (2015); Jiang (2015b); Jain and McGaughey (2015); Zhang et al. (2016a) Fig. 179 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 359. The parameters for the three-body SW potential used by GULP are shown in Tab. 360. Parameters for the SW potential used by LAMMPS are listed in Tab. 361.
Fig. 180 shows the stress strain relations for the black phosphorus of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 24.3 Nm*-1* and 90.5 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. These values agree quite well with previously reported ab initio results, eg. 28.9 Nm*-1* and 101.6 Nm*-1* from Ref. Qiao et al., 2014, or 24.4 Nm*-1* and 92.1 Nm*-1* from Ref. Wei and Peng, 2014, or 24.3 Nm*-1* and 80.2 Nm*-1* from Ref. Qin et al., 2014. The ultimate stress is about 4.27 Nm*-1* at the critical strain of 0.33 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.0 Nm*-1* at the critical strain of 0.19 in the zigzag direction at the low temperature of 1 K. These values agree quite well with the ab initio results at 0 K.Wei and Peng (2014)
It should be noted that the Poisson’s ratios from the VFF model and the SW potential are and . These values are obviously smaller than first-principles calculations results, eg. 0.4 and 0.93 from Ref. Jiang and Park, 2014, or 0.17 and 0.62 from Ref. Qin et al., 2014, or 0.24 and 0.81 from Ref. Elahi et al., 2014. The Poisson’s ratio can not be obtained correctly by the VFF model proposed in 1982Kaneta, Katayama-Yoshida, and Morita (1982) and the SW potentialJiang (2015a) either.Midtvedt and Croy (2016) These failures are due to the missing of one angle-angle crossing term,Jiang (2016) which has not been implemented in the package LAMMPS and is not included in the present work.
XCI p-arsenene
Present studies on the puckered (p-) arsenene, also named arsenene, are based on first-principles calculations, and no empirical potential has been proposed for the p-arsenene. We will thus parametrize a set of VFF model for the single-layer p-arsenene in this section. We will also derive the SW potential based on the VFF model for the single-layer p-arsenene.
The structure of the single-layer p-arsenene is exactly the same as that of the black phosphorus as shown in Fig. 178. Structural parameters for p-arsenene are from the ab initio calculations.Xu et al. (2016) The pucker of the p-arsenene is perpendicular to the x (armchair)-direction. The bases for the rectangular unit cell are Å and Å. There are four As atoms in the basic unit cell, and their relative coordinates are , , , and with and . The value of the dimensionless parameter is extracted from the geometrical parameters provided in Ref. Xu et al., 2016. The other dimensionless parameter is a ratio based on the lattice constant in the out-of-plane z-direction, so the other basis Å from Ref. Zhang et al., 2015 is also adopted in extracting the value of . We note that the main purpose of the usage of and in representing atomic coordinates is to follow the same convention for all puckered structures. The resultant atomic coordinates are the same as that in Ref. Xu et al., 2016.
Table 362 shows four VFF terms for the single-layer p-arsenene, two of which are the bond stretching interactions shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). The force constant parameters are reasonably chosen to be the same for the two bond stretching terms denoted by and , as these two bonds have very close bond length value. The force constant parameters happen to be the same for the two angle bending terms and . These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the X as shown in Fig. 181 (a). The ab initio calculations for the phonon dispersion are from Ref. Xu et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Kamal and Ezawa (2015); Zeraati et al. (2015); Yang and Liu (2016); Zhang et al. (2016a) We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 181 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 363. The parameters for the three-body SW potential used by GULP are shown in Tab. 364. Parameters for the SW potential used by LAMMPS are listed in Tab. 365.
Fig. 182 shows the stress strain relations for the p-arsenene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 20.7 Nm*-1* and 73.0 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -56.4 N/m and -415.5 N/m at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.5 Nm*-1* at the critical strain of 0.31 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.5 Nm*-1* at the critical strain of 0.18 in the zigzag direction at the low temperature of 1 K.
XCII p-antimonene
Present studies on the puckered (p-) antimonene, also named antimonene, are based on first-principles calculations, and no empirical potential has been proposed for the p-antimonene. We will thus parametrize a set of VFF model for the single-layer p-antimonene in this section. We will also derive the SW potential based on the VFF model for the single-layer p-antimonene.
The structure of the single-layer p-antimonene is shown in Fig. 183, which is similar as that of the black phosphorus as shown in Fig. 178. Structural parameters for p-antimonene are from the ab initio calculations.Xu et al. (2016) The pucker of the p-antimonene is perpendicular to the x (armchair)-direction. The bases for the rectangular unit cell are Å and Å. There are four Sb atoms in the basic unit cell, and their relative coordinates are , , , and with , and . The value of the dimensionless parameter is extracted from the geometrical parameters (bond lengths and bond angles) provided in Ref. Xu et al., 2016. The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, so an arbitrary value of Å is adopted in extracting the values of and . The value of has no effect on the actual position of each Sb atom. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention of black phosphorus. The resultant atomic coordinates are the same as that in Ref. Xu et al., 2016.
As shown in Fig. 183 (b), a specific feature in the puckered configuration of the p-antimonene is that Sb atoms in the top/bottom group are further divided into two subgroups with different z-coordinates. Specifically, in Fig. 183 (c), there is a difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. As a result of the nonzero value of , there are two different inter-group angles, i.e., and . We have for the ideal puckered configuration of the black phosphorus.
Table 366 shows five VFF terms for the single-layer p-antimonene, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are reasonably chosen to be the same for the two bond stretching terms denoted by and , as these two bonds have very close bond length value. The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. As a result, there are only three force constant parameters, i.e., , , and . These three force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the X as shown in Fig. 185 (a). The ab initio calculations for the phonon dispersion are from Ref. Xu et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Wang, Pandey, and Karna (2015); Zheng et al. (2016); Zhang et al. (2016a) We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 185 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 367. The parameters for the three-body SW potential used by GULP are shown in Tab. 368. Parameters for the SW potential used by LAMMPS are listed in Tab. 369. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 184, which technically increases the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 183 (c).
Fig. 186 shows the stress strain relations for the p-antimonene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 18.3 Nm*-1* and 65.2 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -22.1 N/m and -354.1 N/m at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.7 Nm*-1* at the critical strain of 0.37 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.4 Nm*-1* at the critical strain of 0.17 in the zigzag direction at the low temperature of 1 K.
XCIII p-bismuthene
Present studies on the puckered (p-) bismuthene, which is also named bismuthene, are based on first-principles calculations, and no empirical potential has been proposed for the p-bismuthene. We will thus parametrize a set of VFF model for the single-layer p-bismuthene in this section. We will also derive the SW potential based on the VFF model for the single-layer p-bismuthene.
The structure of the single-layer p-bismuthene is the same as p-antimonene as shown in Fig. 183. Structural parameters for p-bismuthene are from the ab initio calculations.Akturk, Akturk, and Ciraci (2016) The pucker of the p-bismuthene is perpendicular to the x (armchair)-direction. The bases for the rectangular unit cell are Å and Å. There are four Bi atoms in the basic unit cell, and their relative coordinates are , , , and with , and . The value of the dimensionless parameter is extracted from the geometrical parameters provided in Ref. Akturk, Akturk, and Ciraci, 2016. The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, so an arbitrary value of Å is adopted in extracting the values of and . The value of has no effect on the actual position of each Bi atom. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention of black phosphorus. The resultant atomic coordinates are the same as that in Ref. Akturk, Akturk, and Ciraci, 2016.
As shown in Fig. 183 (b), a specific feature in the puckered configuration of the p-bismuthene is that Bi atoms in the top/bottom group are further divided into two subgroups with different z-coordinates. Specifically, in Fig. 183 (c), there is a difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. As a result of the nonzero value of , there are two different inter-group angles, i.e., and . We have for the ideal puckered configuration of the black phosphorus.
Table 370 shows five VFF terms for the single-layer p-bismuthene, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are reasonably chosen to be the same for the two bond stretching terms denoted by and , as these two bonds have very close bond length value. The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. As a result, there are only three force constant parameters, i.e., , , and . These three force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the X as shown in Fig. 187 (a). The ab initio calculations for the phonon dispersion are from Ref. Akturk, Akturk, and Ciraci, 2016. Similar phonon dispersion can also be found in other ab initio calculations.Zhang et al. (2016a) Fig. 187 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 371. The parameters for the three-body SW potential used by GULP are shown in Tab. 372. Parameters for the SW potential used by LAMMPS are listed in Tab. 373. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 184, which helps to increase the cutoff for the bond stretching interaction between atoms like 1 and 2 in Fig. 183 (c).
Fig. 188 shows the stress strain relations for the p-bismuthene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 10.2 Nm*-1* and 26.2 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . These values are very close to the ab initio calculations, eg. and in Ref. Akturk, Akturk, and Ciraci, 2016. The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -12.4 N/m and -86.4 N/m at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.6 Nm*-1* at the critical strain of 0.38 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.9 Nm*-1* at the critical strain of 0.29 in the zigzag direction at the low temperature of 1 K.
XCIV p-SiO
Present studies on the puckered (p-) SiO are based on first-principles calculations, and no empirical potential has been proposed for the p-SiO. We will thus parametrize the SW potential for the single-layer p-SiO in this section.
The structure of the single-layer p-SiO is shown in Fig. 189, with M=Si and X=O. Structural parameters for p-SiO are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SiO is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for . The p-SiO has a zigzag configuration as shown in Fig. 191, which is a specific case of the puckered structure shown in Fig. 189.
Table 374 shows five VFF terms for the single-layer p-SiO, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 192 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 192 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 375. The parameters for the three-body SW potential used by GULP are shown in Tab. 376. Parameters for the SW potential used by LAMMPS are listed in Tab. 377.
Fig. 193 shows the stress strain relations for the single-layer p-SiO of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The structure of p-SiO is so soft along the armchair direction that the Young’s modulus is almost zero in the armchair direction. The Young’s modulus is 81.3 Nm*-1* in the zigzag direction at 1 K, which is obtained by linear fitting of the stress strain relations in [0, 0.01]. The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The value of is -432.4 Nm*-1* at 1 K along the zigzag direction. The ultimate stress is about 5.3 Nm*-1* at the critical strain of 0.29 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.8 Nm*-1* at the critical strain of 0.23 in the zigzag direction at the low temperature of 1 K.
XCV p-GeO
Present studies on the puckered (p-) GeO are based on first-principles calculations, and no empirical potential has been proposed for the p-GeO. We will thus parametrize the SW potential for the single-layer p-GeO in this section.
The structure of the single-layer p-GeO is shown in Fig. 189, with M=Ge and X=O. Structural parameters for p-GeO are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-GeO is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for . The p-GeO has a zigzag configuration as shown in Fig. 191, which is a specific case of the puckered structure shown in Fig. 189.
Table 378 shows five VFF terms for the single-layer p-GeO, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 194 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 194 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 379. The parameters for the three-body SW potential used by GULP are shown in Tab. 380. Parameters for the SW potential used by LAMMPS are listed in Tab. 381.
Fig. 195 shows the stress strain relations for the single-layer p-GeO of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The structure of p-GeO is so soft along the armchair direction that the Young’s modulus is almost zero in the armchair direction. The Young’s modulus is 14.5 Nm*-1* and 78.9 Nm*-1* in the armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are 22.0 Nm*-1* and -383.3 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 4.8 Nm*-1* at the critical strain of 0.32 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.2 Nm*-1* at the critical strain of 0.23 in the zigzag direction at the low temperature of 1 K.
XCVI p-SnO
Present studies on the puckered (p-) SnO are based on first-principles calculations, and no empirical potential has been proposed for the p-SnO. We will thus parametrize the SW potential for the single-layer p-SnO in this section.
The structure of the single-layer p-SnO is shown in Fig. 189, with M=Sn and X=O. Structural parameters for p-SnO are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SnO is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for . The p-SnO has a zigzag configuration as shown in Fig. 191, which is a specific case of the puckered structure shown in Fig. 189.
Table 382 shows five VFF terms for the single-layer p-SnO, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 196 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 196 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 383. The parameters for the three-body SW potential used by GULP are shown in Tab. 384. Parameters for the SW potential used by LAMMPS are listed in Tab. 385.
Fig. 197 shows the stress strain relations for the single-layer p-SnO of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The structure of p-SnO is so soft along the armchair direction that the Young’s modulus is almost zero in the armchair direction. The Young’s modulus is 52.8 Nm*-1* in the zigzag direction at 1 K, which is obtained by linear fitting of the stress strain relations in [0, 0.01]. The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The value of is -204.5 Nm*-1* at 1 K along the zigzag direction. The ultimate stress is about 3.8 Nm*-1* at the critical strain of 0.38 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.8 Nm*-1* at the critical strain of 0.26 in the zigzag direction at the low temperature of 1 K.
XCVII p-CS
Present studies on the puckered (p-) CS are based on first-principles calculations, and no empirical potential has been proposed for the p-CS. We will thus parametrize the SW potential for the single-layer p-CS in this section.
The structure of the single-layer p-CS is shown in Fig. 189, with M=C and X=S. Structural parameters for p-CS are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-CS is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 386 shows five VFF terms for the single-layer p-CS, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 198 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital bacs set is adopted. Fig. 198 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 387. The parameters for the three-body SW potential used by GULP are shown in Tab. 388. Parameters for the SW potential used by LAMMPS are listed in Tab. 389.
Fig. 199 shows the stress strain relations for the single-layer p-CS of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. There is a structural transition around 0.16 at 1 K, where the C atom is twisted. The Young’s modulus is 16.2 Nm*-1* and 70.5 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -27.3 Nm*-1* and -447.2 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 4.3 Nm*-1* at the critical strain of 0.38 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.2 Nm*-1* at the critical strain of 0.22 in the zigzag direction at the low temperature of 1 K.
XCVIII p-SiS
Present studies on the puckered (p-) SiS are based on first-principles calculations, and no empirical potential has been proposed for the p-SiS. We will thus parametrize the SW potential for the single-layer p-SiS in this section.
The structure of the single-layer p-SiS is shown in Fig. 189, with M=Si and X=S. Structural parameters for p-SiS are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SiS is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 390 shows five VFF terms for the single-layer p-SiS, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 200 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 200 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 391. The parameters for the three-body SW potential used by GULP are shown in Tab. 392. Parameters for the SW potential used by LAMMPS are listed in Tab. 393.
Fig. 201 shows the stress strain relations for the single-layer p-SiS of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 10.9 Nm*-1* and 34.8 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -24.1 Nm*-1* and -145.2 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.3 Nm*-1* at the critical strain of 0.39 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.2 Nm*-1* at the critical strain of 0.25 in the zigzag direction at the low temperature of 1 K.
XCIX p-GeS
Present studies on the puckered (p-) GeS are based on first-principles calculations, and no empirical potential has been proposed for the p-GeS. We will thus parametrize the SW potential for the single-layer p-GeS in this section.
The structure of the single-layer p-GeS is shown in Fig. 189, with M=Ge and X=S. Structural parameters for p-GeS are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-GeS is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 394 shows five VFF terms for the single-layer p-GeS, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 202 (a). The ab initio calculations are from Ref. Qin et al., 2016. Fig. 202 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 395. The parameters for the three-body SW potential used by GULP are shown in Tab. 396. Parameters for the SW potential used by LAMMPS are listed in Tab. 397. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Ge and X=S, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 203 shows the stress strain relations for the single-layer p-GeS of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 10.6 Nm*-1* and 32.1 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -20.4 Nm*-1* and -118.8 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.4 Nm*-1* at the critical strain of 0.39 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.2 Nm*-1* at the critical strain of 0.24 in the zigzag direction at the low temperature of 1 K.
C p-SnS
Present studies on the puckered (p-) SnS are based on first-principles calculations, and no empirical potential has been proposed for the p-SnS. We will thus parametrize the SW potential for the single-layer p-SnS in this section.
The structure of the single-layer p-SnS is shown in Fig. 189, with M=Sn and X=S. Structural parameters for p-SnS are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SnS is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 398 shows five VFF terms for the single-layer p-SnS, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 204 (a). The ab initio calculations are from Ref. Qin et al., 2016. Fig. 204 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 399. The parameters for the three-body SW potential used by GULP are shown in Tab. 400. Parameters for the SW potential used by LAMMPS are listed in Tab. 401. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Sn and X=S, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 205 shows the stress strain relations for the single-layer p-SnS of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 9.6 Nm*-1* and 24.5 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -14.7 Nm*-1* and -80.3 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.3 Nm*-1* at the critical strain of 0.36 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.1 Nm*-1* at the critical strain of 0.20 in the zigzag direction at the low temperature of 1 K.
CI p-CSe
Present studies on the puckered (p-) CSe are based on first-principles calculations, and no empirical potential has been proposed for the p-CSe. We will thus parametrize the SW potential for the single-layer p-CSe in this section.
The structure of the single-layer p-CSe is shown in Fig. 189, with M=C and X=Se. Structural parameters for p-CSe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-CSe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 402 shows five VFF terms for the single-layer p-CSe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 206 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 206 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 403. The parameters for the three-body SW potential used by GULP are shown in Tab. 404. Parameters for the SW potential used by LAMMPS are listed in Tab. 405. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=C and X=Se, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 207 shows the stress strain relations for the single-layer p-CSe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 17.2 Nm*-1* and 75.4 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -46.3 Nm*-1* and -442.0 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.0 Nm*-1* at the critical strain of 0.31 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.5 Nm*-1* at the critical strain of 0.20 in the zigzag direction at the low temperature of 1 K.
CII p-SiSe
Present studies on the puckered (p-) SiSe are based on first-principles calculations, and no empirical potential has been proposed for the p-SiSe. We will thus parametrize the SW potential for the single-layer p-SiSe in this section.
The structure of the single-layer p-SiSe is shown in Fig. 189, with M=Si and X=Se. Structural parameters for p-SiSe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SiSe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 406 shows five VFF terms for the single-layer p-SiSe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 208 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 208 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 407. The parameters for the three-body SW potential used by GULP are shown in Tab. 408. Parameters for the SW potential used by LAMMPS are listed in Tab. 409. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Si and X=Se, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 209 shows the stress strain relations for the single-layer p-SiSe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 14.4 Nm*-1* and 44.6 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -28.8 Nm*-1* and -176.6 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.1 Nm*-1* at the critical strain of 0.37 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.3 Nm*-1* at the critical strain of 0.21 in the zigzag direction at the low temperature of 1 K.
CIII p-GeSe
Present studies on the puckered (p-) GeSe are based on first-principles calculations, and no empirical potential has been proposed for the p-GeSe. We will thus parametrize the SW potential for the single-layer p-GeSe in this section.
The structure of the single-layer p-GeSe is shown in Fig. 189, with M=Ge and X=Se. Structural parameters for p-GeSe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-GeSe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 410 shows five VFF terms for the single-layer p-GeSe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 210 (a). The ab initio calculations are from Ref. Qin et al., 2016. Fig. 210 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 411. The parameters for the three-body SW potential used by GULP are shown in Tab. 412. Parameters for the SW potential used by LAMMPS are listed in Tab. 413. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Ge and X=Se, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 211 shows the stress strain relations for the single-layer p-GeSe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 11.1 Nm*-1* and 32.0 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -19.3 Nm*-1* and -114.7 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.6 Nm*-1* at the critical strain of 0.36 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.9 Nm*-1* at the critical strain of 0.20 in the zigzag direction at the low temperature of 1 K.
CIV p-SnSe
Present studies on the puckered (p-) SnSe are based on first-principles calculations, and no empirical potential has been proposed for the p-SnSe. We will thus parametrize the SW potential for the single-layer p-SnSe in this section.
The structure of the single-layer p-SnSe is shown in Fig. 189, with M=Sn and X=Se. Structural parameters for p-SnSe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SnSe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 414 shows five VFF terms for the single-layer p-SnSe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 212 (a). The ab initio calculations are from Ref. Zhang et al., 2016b. Fig. 212 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 415. The parameters for the three-body SW potential used by GULP are shown in Tab. 416. Parameters for the SW potential used by LAMMPS are listed in Tab. 417. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Sn and X=Se, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 213 shows the stress strain relations for the single-layer p-SnSe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 11.4 Nm*-1* and 34.1 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -22.0 Nm*-1* and -128.8 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.3 Nm*-1* at the critical strain of 0.32 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.3 Nm*-1* at the critical strain of 0.15 in the zigzag direction at the low temperature of 1 K.
CV p-CTe
Present studies on the puckered (p-) CTe are based on first-principles calculations, and no empirical potential has been proposed for the p-CTe. We will thus parametrize the SW potential for the single-layer p-CTe in this section.
The structure of the single-layer p-CTe is shown in Fig. 189, with M=C and X=Te. Structural parameters for p-CTe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-CTe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 418 shows five VFF terms for the single-layer p-CTe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 214 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 214 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 419. The parameters for the three-body SW potential used by GULP are shown in Tab. 420. Parameters for the SW potential used by LAMMPS are listed in Tab. 421. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=C and X=Te, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 215 shows the stress strain relations for the single-layer p-CTe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 10.8 Nm*-1* and 89.1 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -15.3 Nm*-1* and -419.6 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.0 Nm*-1* at the critical strain of 0.43 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.4 Nm*-1* at the critical strain of 0.21 in the zigzag direction at the low temperature of 1 K.
CVI p-SiTe
Present studies on the puckered (p-) SiTe are based on first-principles calculations, and no empirical potential has been proposed for the p-SiTe. We will thus parametrize the SW potential for the single-layer p-SiTe in this section.
The structure of the single-layer p-SiTe is shown in Fig. 189, with M=Si and X=Te. Structural parameters for p-SiTe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SiTe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 422 shows five VFF terms for the single-layer p-SiTe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 216 (a). The ab initio calculations are from Ref. Chen, Sun, and Jena, 2016. Fig. 216 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 423. The parameters for the three-body SW potential used by GULP are shown in Tab. 424. Parameters for the SW potential used by LAMMPS are listed in Tab. 425. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Si and X=Te, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 217 shows the stress strain relations for the single-layer p-SiTe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 14.0 Nm*-1* and 53.6 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -32.9 Nm*-1* and -183.2 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.2 Nm*-1* at the critical strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.0 Nm*-1* at the critical strain of 0.22 in the zigzag direction at the low temperature of 1 K.
CVII p-GeTe
Present studies on the puckered (p-) GeTe are based on first-principles calculations, and no empirical potential has been proposed for the p-GeTe. We will thus parametrize the SW potential for the single-layer p-GeTe in this section.
The structure of the single-layer p-GeTe is shown in Fig. 189, with M=Ge and X=Te. Structural parameters for p-GeTe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-GeTe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 426 shows five VFF terms for the single-layer p-GeTe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 218 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 218 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 427. The parameters for the three-body SW potential used by GULP are shown in Tab. 428. Parameters for the SW potential used by LAMMPS are listed in Tab. 429. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Ge and X=Te, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 219 shows the stress strain relations for the single-layer p-GeTe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 8.1 Nm*-1* and 41.6 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -10.5 Nm*-1* and -143.7 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.6 Nm*-1* at the critical strain of 0.53 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.3 Nm*-1* at the critical strain of 0.21 in the zigzag direction at the low temperature of 1 K.
CVIII p-SnTe
Present studies on the puckered (p-) SnTe are based on first-principles calculations, and no empirical potential has been proposed for the p-SnTe. We will thus parametrize the SW potential for the single-layer p-SnTe in this section.
The structure of the single-layer p-SnTe is shown in Fig. 189, with M=Sn and X=Te. Structural parameters for p-SnTe are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) There are four atoms in the unit cell with relative coordinates as , , , and with , and . The value of these dimensionless parameters are extracted from the geometrical parameters provided in Ref. Kamal, Chakrabarti, and Ezawa, 2016, including lattice constants Å and Å, bond lengths Å and Å, and the angle . The dimensionless parameters and are ratios based on the lattice constant in the out-of-plane z-direction, which is arbitrarily chosen as Å. We note that the main purpose of the usage of , , and in representing atomic coordinates is to follow the same convention for all puckered structures in the present work. The resultant atomic coordinates are the same as that in Ref. Kamal, Chakrabarti, and Ezawa, 2016.
As shown in Fig. 189, a specific feature in the puckered configuration of the p-SnTe is that there is a small difference of between the z-coordinate of atom 1 and the z-coordinates of atoms 2 and 3. Similarly, atom 4 is higher than atoms 5 and 6 for along the z-direction. The sign of determines which types of atoms take the out-most positions, e.g., atoms 1, 5, and 6 are the out-most atoms if in Fig. 189 (c), while atoms 2, 3, and 4 will take the out-most positions for .
Table 430 shows five VFF terms for the single-layer p-SnTe, two of which are the bond stretching interactions shown by Eq. (1) while the other three terms are the angle bending interaction shown by Eq. (2). The force constant parameters are the same for the two angle bending terms and , which have the same arm lengths. All force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the X as shown in Fig. 220 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 220 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion.
The parameters for the two-body SW potential used by GULP are shown in Tab. 431. The parameters for the three-body SW potential used by GULP are shown in Tab. 432. Parameters for the SW potential used by LAMMPS are listed in Tab. 433. Eight atom types have been introduced for writing the SW potential script used by LAMMPS as shown in Fig. 190 with M=Sn and X=Te, which helps to increase the cutoff for the bond stretching interaction between atom 1 and atom 2 in Fig. 189 (c).
Fig. 221 shows the stress strain relations for the single-layer p-SnTe of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 6.6 Nm*-1* and 38.5 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Poisson’s ratios from the VFF model and the SW potential are and . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -7.2 Nm*-1* and -114.5 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 2.4 Nm*-1* at the critical strain of 0.61 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.3 Nm*-1* at the critical strain of 0.21 in the zigzag direction at the low temperature of 1 K.
CIX Silicene
There have been several empirical potentials available for the silicene. A many-body potential based on the Lennard-Jones and Axilrod-Teller functions was used to describe the interaction within the single-layer silicene.Ince and Erkoc (2011) The modified embedded-atom potentialBaskes (1992) was used by Pei et al to simulate the thermal transport in the single-layer silicnene in 2013.Pei et al. (2013) The environment-dependent interatomic potentialJusto et al. (1998) was also used to simulate the silicene.Chavez-Castillo, Rodriguez-Meza, and Meza-Montes (2015) In particular, the original set of SW parametersStillinger and Weber (1985) for the silicon were found to be not suitable for the planar silicene, so two sets of optimized parameters for the SW potential were proposed to simulate the thermal conductivity in the single-layer silicene in 2014.Zhang et al. (2014b) We will develop a new SW potential to describe the interaction within the silicene in this section, with specific focus on the mechanical properties of the silicene.
The structure of the silicene is shown in Fig. 222, with structural parameters from the ab initio calculations.Ge, Yao, and Lu (2016) The silicene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å and the lattice constant is 3.87 Å, which results in a bond length of 2.279 Å.
Table 434 shows the VFF model for the silicene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 223 (a). The ab initio calculations for the phonon dispersion are from Ref. Ge, Yao, and Lu, 2016. Similar phonon dispersion can also be found in other ab initio calculations.Li et al. (2013); Scalise et al. (2013); Roome and Carey (2014); Yang et al. (2014); Wang et al. (2014); Xie, Hu, and Bao (2014); Gu and Yang (2015); Huang, Gong, and Zeng (2015); Wang, Feng, and Ruan (2015); Ge, Yao, and Lu (2016); Xie et al. (2016); Kuang et al. (2016); Peng et al. (2016a) Fig. 223 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
We note that the present SW potential is fitted perfectly to the three acoustic phonon branches, so it can give a nice description for the elastic deformation of the silicene. As a trade off, the optical phonons are overestimated by the present SW potential. Hence, the present SW potential is in particular suitable for the simulation of mechanical or thermal processes which are dominated by acoustic phonons, while the present SW potential may cause a systematic error for the optical absorption process which mainly involves the optical phonons. One can introduce the long-range interactions (eg. the second-nearest-neighboring interaction) to give a good description for both acoustic and optical phonon branches, see one such example for borophene in Ref. Zhou and Jiang, 2017. It is because the long-range interaction mainly contributes to the acoustic phonon branches, while it makes only neglectable contribution to the optical phonon branches. As another solution, the SW potential can give reasonable descriptions for the optical phonon branches by reducing its accuracy in describing acoustic phonon branches as done in Ref. Zhang et al., 2014b.
The parameters for the two-body SW potential used by GULP are shown in Tab. 435. The parameters for the three-body SW potential used by GULP are shown in Tab. 436. Parameters for the SW potential used by LAMMPS are listed in Tab. 437.
Fig. 224 shows the stress strain relations for the silicene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 63.3 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the silicene. The value of the Young’s modulus agrees with the value of 63.8 Nm*-1* from the ab initio calculations.Peng, Wen, and De (2013) The Poisson’s ratios from the VFF model and the SW potential are , which are smaller but comparable with the ab initio results of 0.325.Peng, Wen, and De (2013) The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -212.5 Nm*-1* and -267.5 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 8.6 Nm*-1* at the critical strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.8 Nm*-1* at the critical strain of 0.23 in the zigzag direction at the low temperature of 1 K.
The stress-strain curves shown in Fig. 224 disclose a structural transition at the strain around 0.076 for the silicene at the low temperature of 1 K. The buckled configuration of the silicene is flattened during this structural transition, which can be seen from these two insets in Fig. 224. This structural transition was also observed in the ab initio calculations,Wang et al. (2014) where the critical strain for the structural transition is 0.2. At temperatures above 300 K, this structural transition is blurred by stronger thermal vibrations; i.e., the buckled configuration of the silicene can be strongly disturbed by the thermal vibration at higher temperatures.
CX Germanene
In a recent work, the Tersoff potential was applied to simulate the thermal conductivity of the germanene nanoribbon.Balatero et al. (2015) We will provide the SW potential to describe the interaction within the germanene in this section.
The structure of the germanene is shown in Fig. 222, with structural parameters from the ab initio calculations.Ge, Yao, and Lu (2016) The germanene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å and the lattice constant is 4.06 Å, which results in a bond length of 2.443 Å.
Table 438 shows the VFF model for the germanene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 225 (a). The ab initio calculations for the phonon dispersion are from Ref. Ge, Yao, and Lu, 2016. Similar phonon dispersion can also be found in other ab initio calculations.Scalise et al. (2013); Roome and Carey (2014); Huang, Gong, and Zeng (2015); Ge, Yao, and Lu (2016); Kuang et al. (2016); Zaveh, Roknabadi, and T. Morshedloo (2016); Peng et al. (2016a) Fig. 225 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 439. The parameters for the three-body SW potential used by GULP are shown in Tab. 440. Parameters for the SW potential used by LAMMPS are listed in Tab. 441.
Fig. 226 shows the stress strain relations for the germanene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 53.2 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the germanene. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -229.2 Nm*-1* and -278.2 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 7.5 Nm*-1* at the critical strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.3 Nm*-1* at the critical strain of 0.27 in the zigzag direction at the low temperature of 1 K.
The stress-strain curves shown in Fig. 226 disclose a structural transition for the germanene at the low temperature of 1 K. The critical strains for the structural transition are 0.15 and 0.16 along the armchair and zigzag directions, respectively. The buckled configuration of the germanene is flattened during this structural transition, which can be seen from these two insets in Fig. 226. At temperatures above 300 K, this structural transition is blurred by stronger thermal vibrations; i.e., the buckled configuration of the germanene can be strongly disturbed by the thermal vibration at higher temperatures.
CXI Stanene
There are several available empirical potentials for the description of the interaction within the stanene. The modified embedded atom method potential was applied to simulate mechanical properties for the stanene.Mojumder, Amin, and Islam (2015) A VFF model was fitted for the stanene in 2015.Modarresi et al. (2015) The Tersoff potential was parameterized to describe the interaction for stanene.Cherukara et al. (2016) In this section, we will develop the SW potential for the stanene.
The structure of the stanene is shown in Fig. 222, with structural parameters from the ab initio calculations.Zaveh, Roknabadi, and T. Morshedloo (2016) The stanene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å and the lattice constant is 4.68 Å, which results in a bond length of 2.836 Å.
Table 442 shows the VFF model for the stanene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 227 (a). The ab initio calculations for the phonon dispersion are from Ref. Zaveh, Roknabadi, and T. Morshedloo, 2016 with the spin-orbit coupling effect. Similar phonon dispersion can also be found in other ab initio calculations.van den Broek et al. (2014); Kuang et al. (2016); Zaveh, Roknabadi, and T. Morshedloo (2016); Peng et al. (2016b); Zhou et al. (2016); Peng et al. (2016a) Fig. 227 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 443. The parameters for the three-body SW potential used by GULP are shown in Tab. 444. Parameters for the SW potential used by LAMMPS are listed in Tab. 445.
Fig. 228 shows the stress strain relations for the stanene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 17.0 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the stanene. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -37.2 Nm*-1* and -69.4 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 3.5 Nm*-1* at the critical strain of 0.32 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.6 Nm*-1* at the critical strain of 0.29 in the zigzag direction at the low temperature of 1 K.
The stress-strain curves shown in Fig. 228 disclose a structural transition for the stanene at the low temperature of 1 K. The critical strain for the structural transition is about 0.15 along the armchair and zigzag directions. The buckled configuration of the stanene is flattened during this structural transition, which can be seen from these two insets in Fig. 228. At temperatures above 300 K, this structural transition is blurred by stronger thermal vibrations; i.e., the buckled configuration of the stanene can be strongly disturbed by the thermal vibration at higher temperatures.
CXII Indiene
In this section, we will develop the SW potential for the indiene, i.e., the single layer of Indium atoms. The structure of the indiene is shown in Fig. 222, with structural parameters from the ab initio calculations.Singh et al. (2016) The indiene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The lattice constant is 4.24 Å and the bond length is 2.89 Å, which results in the buckling height of Å.
Table 446 shows the VFF model for the indiene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 229 (a). The ab initio calculations for the phonon dispersion are from Ref. Singh et al., 2016. We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 229 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 447. The parameters for the three-body SW potential used by GULP are shown in Tab. 448. Parameters for the SW potential used by LAMMPS are listed in Tab. 449.
Fig. 230 shows the stress strain relations for the indiene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K. The Young’s modulus is 8.4 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus of the indiene is very small; i.e., the indiene is very soft. As a result, we find that the structure becomes unstable at room temperature. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -42.0 Nm*-1* and -50.2 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 0.77 Nm*-1* at the critical strain of 0.16 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 0.73 Nm*-1* at the critical strain of 0.19 in the zigzag direction at the low temperature of 1 K.
CXIII Blue phosphorus
The blue phosphorus is also named -phosphorus. Present studies on the blue phosphorus are based on first-principles calculations, and no empirical potential has been proposed for the blue phosphorus. We will thus parametrize a set of VFF model for the single-layer blue phosphorus in this section. We will also derive the SW potential based on the VFF model for the single-layer blue phosphorus.
The structure of the single-layer blue phosphorus is shown in Fig. 222, with structural parameters from the ab initio calculations.Zhu and Tomanek (2014) The blue phosphorus has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å. The lattice constant is 3.326 Å, and the bond length is 2.270 Å.
Table 450 shows the VFF model for the single-layer blue phosphorus. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 231 (a). The ab initio calculations for the phonon dispersion are from Ref. Zhu and Tomanek, 2014. Similar phonon dispersion can also be found in other ab initio calculations.Aierken et al. (2015); Ge, Yao, and Lu (2016); Zhang et al. (2016a) Fig. 231 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 451. The parameters for the three-body SW potential used by GULP are shown in Tab. 452. Parameters for the SW potential used by LAMMPS are listed in Tab. 453.
Fig. 232 shows the stress strain relations for the single-layer blue phosphorus of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 60.5 Nm*-1* and 60.6 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the blue phosphorus. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -195.3 Nm*-1* and -237.0 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 8.0 Nm*-1* at the critical strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.6 Nm*-1* at the critical strain of 0.25 in the zigzag direction at the low temperature of 1 K.
CXIV b-arsenene
Present studies on the buckled (b-) arsenene, whch is also named arsenene, are based on first-principles calculations, and no empirical potential has been proposed for the b-arsenene. We will thus parametrize a set of VFF model for the single-layer b-arsenene in this section. We will also derive the SW potential based on the VFF model for the single-layer b-arsenene.
The structure of the single-layer b-arsenene is shown in Fig. 222, with structural parameters from the ab initio calculations.Xu et al. (2016) The b-arsenene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å. The lattice constant is 3.61 Å, and the bond length is 2.51 Å.
Table 454 shows the VFF model for the single-layer b-arsenene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 233 (a). The ab initio calculations for the phonon dispersion are from Ref. Xu et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Kamal and Ezawa (2015); Zeraati et al. (2015); Zhang et al. (2016a) We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 233 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 455. The parameters for the three-body SW potential used by GULP are shown in Tab. 456. Parameters for the SW potential used by LAMMPS are listed in Tab. 457.
Fig. 234 shows the stress strain relations for the single-layer b-arsenene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 50.8 Nm*-1* and 49.9 Nm*-1* in the armchair and zigzag directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the b-arsenene. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -127.6 Nm*-1* and -153.6 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 7.6 Nm*-1* at the critical strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.2 Nm*-1* at the critical strain of 0.28 in the zigzag direction at the low temperature of 1 K.
CXV b-antimonene
The buckled (b-) antimonene is a Sb allotrope, which is also named antimonene. Present studies on the b-antimonene are based on first-principles calculations, and no empirical potential has been proposed for the b-antimonene. We will thus parametrize a set of VFF model for the single-layer b-antimonene in this section. We will also derive the SW potential based on the VFF model for the single-layer b-antimonene.
The structure of the single-layer b-antimonene is shown in Fig. 222, with structural parameters from the ab initio calculations.Xu et al. (2016) The b-antimonene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å. The lattice constant is 4.12 Å, and the bond length is 2.89 Å.
Table 458 shows the VFF model for the single-layer b-antimonene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 235 (a). The ab initio calculations for the phonon dispersion are from Ref. Xu et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Kamal and Ezawa (2015); Zeraati et al. (2015); Zhang et al. (2016a) Fig. 235 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 459. The parameters for the three-body SW potential used by GULP are shown in Tab. 460. Parameters for the SW potential used by LAMMPS are listed in Tab. 461.
Fig. 236 shows the stress strain relations for the single-layer b-antimonene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 39.6 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the b-antimonene. The Poisson’s ratios from the VFF model and the SW potential are . The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -62.6 Nm*-1* and -91.5 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 7.1 Nm*-1* at the critical strain of 0.28 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.7 Nm*-1* at the critical strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXVI b-bismuthene
The buckled (b-) bismuthene is a Bi allotrope, which is also named bismuthene. Most studies on the b-bismuthene are based on first-principles calculations, while a modified Morse potential was proposed for the b-bismuthene in 2013.Cheng et al. (2013) We will parametrize a set of VFF model for the single-layer b-bismuthene in this section. We will also derive the SW potential based on the VFF model for the single-layer b-bismuthene.
The structure of the single-layer b-bismuthene is shown in Fig. 222, with structural parameters from the ab initio calculations.Xu et al. (2016) The b-bismuthene has a buckled configuration as shown in Fig. 222 (b), where the buckle is along the zigzag direction. The height of the buckle is Å. The lattice constant is 4.34 Å, and the bond length is 3.045 Å.
Table 462 shows the VFF model for the single-layer b-bismuthene. The force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the M as shown in Fig. 237 (a). The ab initio calculations for the phonon dispersion are from Ref. Zhang et al., 2016a. Similar phonon dispersion can also be found in other ab initio calculations.Akturk, Akturk, and Ciraci (2016) We note that the lowest-frequency branch aroung the point from the VFF model is lower than the ab initio results. This branch is the flexural branch, which should be a quadratic dispersion. However, the ab initio calculations give a linear dispersion for the flexural branch due to the violation of the rigid rotational invariance in the first-principles package,Jiang et al. (2015) so ab initio calculations typically overestimate the frequency of this branch. Fig. 237 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 463. The parameters for the three-body SW potential used by GULP are shown in Tab. 464. Parameters for the SW potential used by LAMMPS are listed in Tab. 465.
Fig. 238 shows the stress strain relations for the single-layer b-bismuthene of size Å. The structure is uniaxially stretched in the armchair or zigzag directions at 1 K and 300 K. The Young’s modulus is 27.0 Nm*-1* in both armchair and zigzag directions at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. The Young’s modulus is isotropic for the b-bismuthene. The value of the Young’s modulus is close to the value of 23.9 Nm*-1* from the ab initio calculations.Akturk, Akturk, and Ciraci (2016) The Poisson’s ratios from the VFF model and the SW potential are , which are comparable with the ab initio results of 0.327.Akturk, Akturk, and Ciraci (2016) The third-order nonlinear elastic constant can be obtained by fitting the stress-strain relation to with E as the Young’s modulus. The values of are -34.3 Nm*-1* and -54.5 Nm*-1* at 1 K along the armchair and zigzag directions, respectively. The ultimate stress is about 5.2 Nm*-1* at the critical strain of 0.29 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.9 Nm*-1* at the critical strain of 0.33 in the zigzag direction at the low temperature of 1 K.
CXVII b-CO
Present studies on the buckled (b-) CO are based on first-principles calculations, and no empirical potential has been proposed for the b-CO. We will thus parametrize a set of SW potential for the single-layer b-CO in this section.
The structure of the single-layer b-CO is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-CO has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 2.454 Å and the bond length 1.636 Å.
Table 466 shows the VFF model for the single-layer b-CO. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 240 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 240 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 467. The parameters for the three-body SW potential used by GULP are shown in Tab. 468. Parameters for the SW potential used by LAMMPS are listed in Tab. 469.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-CO under uniaxial tension at 1.0 K and 300.0 K. Fig. 241 shows the stress-strain curve for the tension of a single-layer b-CO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-CO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-CO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 99.1 N/m and 98.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-CO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -513.8 N/m and -542.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.4 Nm*-1* at the ultimate strain of 0.18 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.2 Nm*-1* at the ultimate strain of 0.21 in the zigzag direction at the low temperature of 1 K.
CXVIII b-CS
Present studies on the buckled (b-) CS are based on first-principles calculations, and no empirical potential has been proposed for the b-CS. We will thus parametrize a set of SW potential for the single-layer b-CS in this section.
The structure of the single-layer b-CS is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-CS has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 2.836 Å and the bond length 1.880 Å.
Table 470 shows the VFF model for the single-layer b-CS. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 242 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 242 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 471. The parameters for the three-body SW potential used by GULP are shown in Tab. 472. Parameters for the SW potential used by LAMMPS are listed in Tab. 473.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-CS under uniaxial tension at 1.0 K and 300.0 K. Fig. 243 shows the stress-strain curve for the tension of a single-layer b-CS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-CS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-CS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 63.5 N/m and 63.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-CS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -352.5 N/m and -372.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.7 Nm*-1* at the ultimate strain of 0.17 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.5 Nm*-1* at the ultimate strain of 0.20 in the zigzag direction at the low temperature of 1 K.
CXIX b-CSe
Present studies on the buckled (b-) CSe are based on first-principles calculations, and no empirical potential has been proposed for the b-CSe. We will thus parametrize a set of SW potential for the single-layer b-CSe in this section.
The structure of the single-layer b-CSe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-CSe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.063 Å and the bond length 2.055 Å.
Table 474 shows the VFF model for the single-layer b-CSe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 244 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 244 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 475. The parameters for the three-body SW potential used by GULP are shown in Tab. 476. Parameters for the SW potential used by LAMMPS are listed in Tab. 477.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-CSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 245 shows the stress-strain curve for the tension of a single-layer b-CSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-CSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-CSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 61.6 N/m and 61.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-CSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -306.6 N/m and -324.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.1 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.22 in the zigzag direction at the low temperature of 1 K.
CXX b-CTe
Present studies on the buckled (b-) CTe are based on first-principles calculations, and no empirical potential has been proposed for the b-CTe. We will thus parametrize a set of SW potential for the single-layer b-CTe in this section.
The structure of the single-layer b-CTe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-CTe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.348 Å and the bond length 2.231 Å.
Table 478 shows the VFF model for the single-layer b-CTe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 246 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 246 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 479. The parameters for the three-body SW potential used by GULP are shown in Tab. 480. Parameters for the SW potential used by LAMMPS are listed in Tab. 481.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-CTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 247 shows the stress-strain curve for the tension of a single-layer b-CTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-CTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-CTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 48.8 N/m and 48.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-CTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -306.6 N/m and -324.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.23 in the zigzag direction at the low temperature of 1 K.
CXXI b-SiO
Present studies on the buckled (b-) SiO are based on first-principles calculations, and no empirical potential has been proposed for the b-SiO. We will thus parametrize a set of SW potential for the single-layer b-SiO in this section.
The structure of the single-layer b-SiO is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SiO has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 2.815 Å and the bond length 1.884 Å.
Table 482 shows the VFF model for the single-layer b-SiO. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 248 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 248 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 483. The parameters for the three-body SW potential used by GULP are shown in Tab. 484. Parameters for the SW potential used by LAMMPS are listed in Tab. 485.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SiO under uniaxial tension at 1.0 K and 300.0 K. Fig. 249 shows the stress-strain curve for the tension of a single-layer b-SiO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SiO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SiO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 51.3 N/m and 50.3 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SiO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -247.8 N/m and -253.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.2 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.1 Nm*-1* at the ultimate strain of 0.23 in the zigzag direction at the low temperature of 1 K.
CXXII b-SiS
Present studies on the buckled (b-) SiS are based on first-principles calculations, and no empirical potential has been proposed for the b-SiS. We will thus parametrize a set of SW potential for the single-layer b-SiS in this section.
The structure of the single-layer b-SiS is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SiS has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.299 Å and the bond length 2.321 Å.
Table 486 shows the VFF model for the single-layer b-SiS. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 250 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 250 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 487. The parameters for the three-body SW potential used by GULP are shown in Tab. 488. Parameters for the SW potential used by LAMMPS are listed in Tab. 489.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SiS under uniaxial tension at 1.0 K and 300.0 K. Fig. 251 shows the stress-strain curve for the tension of a single-layer b-SiS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SiS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SiS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 45.5 N/m and 45.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SiS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -196.4 N/m and -217.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.1 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
CXXIII b-SiSe
Present studies on the buckled (b-) SiSe are based on first-principles calculations, and no empirical potential has been proposed for the b-SiSe. We will thus parametrize a set of SW potential for the single-layer b-SiSe in this section.
The structure of the single-layer b-SiSe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SiSe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.521 Å and the bond length 2.477 Å.
Table 490 shows the VFF model for the single-layer b-SiSe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 252 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 252 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 491. The parameters for the three-body SW potential used by GULP are shown in Tab. 492. Parameters for the SW potential used by LAMMPS are listed in Tab. 493.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SiSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 253 shows the stress-strain curve for the tension of a single-layer b-SiSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SiSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SiSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 41.8 N/m and 41.9 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SiSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -169.9 N/m and -188.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.7 Nm*-1* at the ultimate strain of 0.25 in the zigzag direction at the low temperature of 1 K.
CXXIV b-SiTe
Present studies on the buckled (b-) SiTe are based on first-principles calculations, and no empirical potential has been proposed for the b-SiTe. We will thus parametrize a set of SW potential for the single-layer b-SiTe in this section.
The structure of the single-layer b-SiTe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Chen, Sun, and Jena (2016) The b-SiTe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 3.83 Å and the bond length 2.689 Å. The resultant height of the buckle is Å.
Table 494 shows the VFF model for the single-layer b-SiTe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 254 (a). The ab initio calculations for the phonon dispersion are from Ref. Chen, Sun, and Jena, 2016. Fig. 254 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 495. The parameters for the three-body SW potential used by GULP are shown in Tab. 496. Parameters for the SW potential used by LAMMPS are listed in Tab. 497.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SiTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 255 shows the stress-strain curve for the tension of a single-layer b-SiTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SiTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SiTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 34.3 N/m and 34.6 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. These values agrees with the ab initio result at 0 K temperature, eg. 34.1 Nm*-1* in Ref. Chen, Sun, and Jena, 2016. The Poisson’s ratio from the VFF model and the SW potential is , which agrees with the ab initio resultChen, Sun, and Jena (2016) of 0.18.
There is no available value for nonlinear quantities in the single-layer b-SiTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -119.3 N/m and -137.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.6 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.4 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
CXXV b-GeO
Present studies on the buckled (b-) GeO are based on first-principles calculations, and no empirical potential has been proposed for the b-GeO. We will thus parametrize a set of SW potential for the single-layer b-GeO in this section.
The structure of the single-layer b-GeO is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-GeO has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.124 Å and the bond length 2.032 Å.
Table 498 shows the VFF model for the single-layer b-GeO. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 256 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 256 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 499. The parameters for the three-body SW potential used by GULP are shown in Tab. 500. Parameters for the SW potential used by LAMMPS are listed in Tab. 501.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GeO under uniaxial tension at 1.0 K and 300.0 K. Fig. 257 shows the stress-strain curve for the tension of a single-layer b-GeO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GeO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GeO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 47.5 N/m and 46.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GeO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -224.6 N/m and -232.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.20 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.8 Nm*-1* at the ultimate strain of 0.23 in the zigzag direction at the low temperature of 1 K.
CXXVI b-GeS
Present studies on the buckled (b-) GeS are based on first-principles calculations, and no empirical potential has been proposed for the b-GeS. We will thus parametrize a set of SW potential for the single-layer b-GeS in this section.
The structure of the single-layer b-GeS is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-GeS has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.485 Å and the bond length 2.428 Å.
Table 502 shows the VFF model for the single-layer b-GeS. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 258 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 258 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 503. The parameters for the three-body SW potential used by GULP are shown in Tab. 504. Parameters for the SW potential used by LAMMPS are listed in Tab. 505.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GeS under uniaxial tension at 1.0 K and 300.0 K. Fig. 259 shows the stress-strain curve for the tension of a single-layer b-GeS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GeS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GeS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 34.9 N/m and 34.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GeS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -128.1 N/m and -135.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.5 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.3 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
CXXVII b-GeSe
Present studies on the buckled (b-) GeSe are based on first-principles calculations, and no empirical potential has been proposed for the b-GeSe. We will thus parametrize a set of SW potential for the single-layer b-GeSe in this section.
The structure of the single-layer b-GeSe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-GeSe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.676 Å and the bond length 2.568 Å.
Table 506 shows the VFF model for the single-layer b-GeSe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 260 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 260 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 507. The parameters for the three-body SW potential used by GULP are shown in Tab. 508. Parameters for the SW potential used by LAMMPS are listed in Tab. 509.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GeSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 261 shows the stress-strain curve for the tension of a single-layer b-GeSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GeSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GeSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 31.6 N/m and 31.5 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GeSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -105.2 N/m and -118.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.4 Nm*-1* at the ultimate strain of 0.24 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.2 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
CXXVIII b-GeTe
Present studies on the buckled (b-) GeTe are based on first-principles calculations, and no empirical potential has been proposed for the b-GeTe. We will thus parametrize a set of SW potential for the single-layer b-GeTe in this section.
The structure of the single-layer b-GeTe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-GeTe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.939 Å and the bond length 2.768 Å.
Table 510 shows the VFF model for the single-layer b-GeTe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 262 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 262 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 511. The parameters for the three-body SW potential used by GULP are shown in Tab. 512. Parameters for the SW potential used by LAMMPS are listed in Tab. 513.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GeTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 263 shows the stress-strain curve for the tension of a single-layer b-GeTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GeTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GeTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 27.7 N/m and 28.0 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GeTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -80.4 N/m and -95.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.3 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.1 Nm*-1* at the ultimate strain of 0.30 in the zigzag direction at the low temperature of 1 K.
CXXIX b-SnO
Present studies on the buckled (b-) SnO are based on first-principles calculations, and no empirical potential has been proposed for the b-SnO. We will thus parametrize a set of SW potential for the single-layer b-SnO in this section.
The structure of the single-layer b-SnO is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SnO has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.442 Å and the bond length 2.204 Å.
Table 514 shows the VFF model for the single-layer b-SnO. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 264 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 264 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 515. The parameters for the three-body SW potential used by GULP are shown in Tab. 516. Parameters for the SW potential used by LAMMPS are listed in Tab. 517.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnO under uniaxial tension at 1.0 K and 300.0 K. Fig. 265 shows the stress-strain curve for the tension of a single-layer b-SnO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 43.7 N/m and 43.8 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -199.9 N/m and -215.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.7 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 4.5 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
CXXX b-SnS
Present studies on the buckled (b-) SnS are based on first-principles calculations, and no empirical potential has been proposed for the b-SnS. We will thus parametrize a set of SW potential for the single-layer b-SnS in this section.
The structure of the single-layer b-SnS is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SnS has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.757 Å and the bond length 2.616 Å.
Table 518 shows the VFF model for the single-layer b-SnS. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 266 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 266 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 519. The parameters for the three-body SW potential used by GULP are shown in Tab. 520. Parameters for the SW potential used by LAMMPS are listed in Tab. 521.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnS under uniaxial tension at 1.0 K and 300.0 K. Fig. 267 shows the stress-strain curve for the tension of a single-layer b-SnS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 23.8 N/m and 24.4 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -71.8 N/m and -88.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 3.5 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.4 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
CXXXI b-SnSe
Present studies on the buckled (b-) SnSe are based on first-principles calculations, and no empirical potential has been proposed for the b-SnSe. We will thus parametrize a set of SW potential for the single-layer b-SnSe in this section.
The structure of the single-layer b-SnSe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SnSe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 3.916 Å and the bond length 2.747 Å.
Table 522 shows the VFF model for the single-layer b-SnSe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 268 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 268 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 523. The parameters for the three-body SW potential used by GULP are shown in Tab. 524. Parameters for the SW potential used by LAMMPS are listed in Tab. 525.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 269 shows the stress-strain curve for the tension of a single-layer b-SnSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 22.0 N/m and 22.2 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -61.6 N/m and -73.69 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 3.5 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.3 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXXXII b-SnTe
Present studies on the buckled (b-) SnTe are based on first-principles calculations, and no empirical potential has been proposed for the b-SnTe. We will thus parametrize a set of SW potential for the single-layer b-SnTe in this section.
The structure of the single-layer b-SnTe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Kamal, Chakrabarti, and Ezawa (2016) The b-SnTe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, including the lattice constant 4.151 Å and the bond length 2.947 Å.
Table 526 shows the VFF model for the single-layer b-SnTe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 270 (a). The ab initio calculations for the phonon dispersion are calculated from the SIESTA package.Soler et al. (2002) The generalized gradients approximation is applied to account for the exchange-correlation function with Perdew, Burke, and Ernzerhof parameterization,Perdew, Burke, and Ernzerhof (1996) and the double- orbital basis set is adopted. Fig. 270 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 527. The parameters for the three-body SW potential used by GULP are shown in Tab. 528. Parameters for the SW potential used by LAMMPS are listed in Tab. 529.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 271 shows the stress-strain curve for the tension of a single-layer b-SnTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus are 19.6 N/m and 19.1 N/m along the armchair and zigzag directions, respectively. The Young’s modulus is essentially isotropic in the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -48.7 N/m and -54.3 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 3.4 Nm*-1* at the ultimate strain of 0.29 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 3.3 Nm*-1* at the ultimate strain of 0.33 in the zigzag direction at the low temperature of 1 K.
CXXXIII b-SnGe
Present studies on the buckled SnGe (b-SnGe) are based on first-principles calculations, and no empirical potential has been proposed for the b-SnGe. We will thus parametrize a set of SW potential for the single-layer b-SnGe in this section.
The structure of the single-layer b-SnGe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-SnGe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.27 Å and the bond length 2.57 Å. The resultant height of the buckle is Å.
Table 530 shows the VFF model for the single-layer b-SnGe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 272 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 272 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 531. The parameters for the three-body SW potential used by GULP are shown in Tab. 532. Parameters for the SW potential used by LAMMPS are listed in Tab. 533.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnGe under uniaxial tension at 1.0 K and 300.0 K. Fig. 273 shows the stress-strain curve for the tension of a single-layer b-SnGe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnGe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnGe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 36.8 N/m along both armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnGe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -171.6 N/m and -197.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 4.9 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.0 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXXXIV b-SiGe
Present studies on the buckled SiGe (b-SiGe) are based on first-principles calculations, and no empirical potential has been proposed for the b-SiGe. We will thus parametrize a set of SW potential for the single-layer b-SiGe in this section.
The structure of the single-layer b-SiGe is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-SiGe has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 3.89 Å and the bond length 2.31 Å. The resultant height of the buckle is Å.
Table 534 shows the VFF model for the single-layer b-SiGe. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 274 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 274 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 535. The parameters for the three-body SW potential used by GULP are shown in Tab. 536. Parameters for the SW potential used by LAMMPS are listed in Tab. 537.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SiGe under uniaxial tension at 1.0 K and 300.0 K. Fig. 275 shows the stress-strain curve for the tension of a single-layer b-SiGe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SiGe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SiGe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 54.6 N/m and 54.3 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SiGe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -186.7 N/m and -233.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.0 Nm*-1* at the ultimate strain of 0.31 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.2 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXXXV b-SnSi
Present studies on the buckled SnSi (b-SnSi) are based on first-principles calculations, and no empirical potential has been proposed for the b-SnSi. We will thus parametrize a set of SW potential for the single-layer b-SnSi in this section.
The structure of the single-layer b-SnSi is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-SnSi has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.21 Å and the bond length 2.52 Å. The resultant height of the buckle is Å.
Table 538 shows the VFF model for the single-layer b-SnSi. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 276 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 276 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 539. The parameters for the three-body SW potential used by GULP are shown in Tab. 540. Parameters for the SW potential used by LAMMPS are listed in Tab. 541.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-SnSi under uniaxial tension at 1.0 K and 300.0 K. Fig. 277 shows the stress-strain curve for the tension of a single-layer b-SnSi of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-SnSi is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-SnSi. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 39.0 N/m and 38.4 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-SnSi. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -150.5 N/m and -174.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 6.5 Nm*-1* at the ultimate strain of 0.28 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.6 Nm*-1* at the ultimate strain of 0.32 in the zigzag direction at the low temperature of 1 K.
CXXXVI b-InP
Present studies on the buckled InP (b-InP) are based on first-principles calculations, and no empirical potential has been proposed for the b-InP. We will thus parametrize a set of SW potential for the single-layer b-InP in this section.
The structure of the single-layer b-InP is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-InP has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.17 Å and the bond length 2.46 Å. The resultant height of the buckle is Å.
Table 542 shows the VFF model for the single-layer b-InP. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 278 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 278 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 543. The parameters for the three-body SW potential used by GULP are shown in Tab. 544. Parameters for the SW potential used by LAMMPS are listed in Tab. 545.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-InP under uniaxial tension at 1.0 K and 300.0 K. Fig. 279 shows the stress-strain curve for the tension of a single-layer b-InP of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-InP is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-InP. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 39.3 N/m and 38.3 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-InP. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -119.3 N/m and -132.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.2 Nm*-1* at the ultimate strain of 0.35 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 9.1 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXXXVII b-InAs
Present studies on the buckled InAs (b-InAs) are based on first-principles calculations, and no empirical potential has been proposed for the b-InAs. We will thus parametrize a set of SW potential for the single-layer b-InAs in this section.
The structure of the single-layer b-InAs is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-InAs has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.28 Å and the bond length 2.55 Å. The resultant height of the buckle is Å.
Table 546 shows the VFF model for the single-layer b-InAs. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 280 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 280 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 547. The parameters for the three-body SW potential used by GULP are shown in Tab. 548. Parameters for the SW potential used by LAMMPS are listed in Tab. 549.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-InAs under uniaxial tension at 1.0 K and 300.0 K. Fig. 281 shows the stress-strain curve for the tension of a single-layer b-InAs of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-InAs is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-InAs. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 33.9 N/m and 34.2 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-InAs. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -85.0 N/m and -130.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 7.3 Nm*-1* at the ultimate strain of 0.32 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.5 Nm*-1* at the ultimate strain of 0.32 in the zigzag direction at the low temperature of 1 K.
CXXXVIII b-InSb
Present studies on the buckled InSb (b-InSb) are based on first-principles calculations, and no empirical potential has been proposed for the b-InSb. We will thus parametrize a set of SW potential for the single-layer b-InSb in this section.
The structure of the single-layer b-InSb is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-InSb has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.57 Å and the bond length 2.74 Å. The resultant height of the buckle is Å.
Table 550 shows the VFF model for the single-layer b-InSb. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 282 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 282 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 551. The parameters for the three-body SW potential used by GULP are shown in Tab. 552. Parameters for the SW potential used by LAMMPS are listed in Tab. 553.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-InSb under uniaxial tension at 1.0 K and 300.0 K. Fig. 283 shows the stress-strain curve for the tension of a single-layer b-InSb of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-InSb is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-InSb. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 28.6 N/m and 28.9 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-InSb. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -85.4 N/m and -121.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.8 Nm*-1* at the ultimate strain of 0.31 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 6.0 Nm*-1* at the ultimate strain of 0.33 in the zigzag direction at the low temperature of 1 K.
CXXXIX b-GaAs
Present studies on the buckled GaAs (b-GaAs) are based on first-principles calculations, and no empirical potential has been proposed for the b-GaAs. We will thus parametrize a set of SW potential for the single-layer b-GaAs in this section.
The structure of the single-layer b-GaAs is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-GaAs has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 3.97 Å and the bond length 2.36 Å. The resultant height of the buckle is Å.
Table 554 shows the VFF model for the single-layer b-GaAs. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 284 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 284 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 555. The parameters for the three-body SW potential used by GULP are shown in Tab. 556. Parameters for the SW potential used by LAMMPS are listed in Tab. 557.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GaAs under uniaxial tension at 1.0 K and 300.0 K. Fig. 285 shows the stress-strain curve for the tension of a single-layer b-GaAs of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GaAs is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GaAs. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 50.5 N/m and 50.9 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GaAs. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -199.5 N/m and -258.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.3 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.3 Nm*-1* at the ultimate strain of 0.30 in the zigzag direction at the low temperature of 1 K.
CXL b-GaP
Present studies on the buckled GaP (b-GaP) are based on first-principles calculations, and no empirical potential has been proposed for the b-GaP. We will thus parametrize a set of SW potential for the single-layer b-GaP in this section.
The structure of the single-layer b-GaP is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-GaP has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 3.84 Å and the bond length 2.25 Å. The resultant height of the buckle is Å.
Table 558 shows the VFF model for the single-layer b-GaP. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 286 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 286 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 559. The parameters for the three-body SW potential used by GULP are shown in Tab. 560. Parameters for the SW potential used by LAMMPS are listed in Tab. 561.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-GaP under uniaxial tension at 1.0 K and 300.0 K. Fig. 287 shows the stress-strain curve for the tension of a single-layer b-GaP of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-GaP is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-GaP. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 57.2 N/m and 57.4 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-GaP. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -186.4 N/m and -261.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.3 Nm*-1* at the ultimate strain of 0.29 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.9 Nm*-1* at the ultimate strain of 0.29 in the zigzag direction at the low temperature of 1 K.
CXLI b-AlSb
Present studies on the buckled AlSb (b-AlSb) are based on first-principles calculations, and no empirical potential has been proposed for the b-AlSb. We will thus parametrize a set of SW potential for the single-layer b-AlSb in this section.
The structure of the single-layer b-AlSb is shown in Fig. 239. The structural parameters are from the ab initio calculations.Sahin et al. (2009) The b-AlSb has a buckled configuration as shown in Fig. 239 (b), where the buckle is along the zigzag direction. This structure can be determined by two independent geometrical parameters, eg. the lattice constant 4.33 Å and the bond length 2.57 Å. The resultant height of the buckle is Å.
Table 562 shows the VFF model for the single-layer b-AlSb. The force constant parameters are determined by fitting to the acoustic branches in the phonon dispersion along the M as shown in Fig. 288 (a). The ab initio calculations for the phonon dispersion are from Ref. Sahin et al., 2009. Fig. 288 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 563. The parameters for the three-body SW potential used by GULP are shown in Tab. 564. Parameters for the SW potential used by LAMMPS are listed in Tab. 565.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer b-AlSb under uniaxial tension at 1.0 K and 300.0 K. Fig. 289 shows the stress-strain curve for the tension of a single-layer b-AlSb of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer b-AlSb is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer b-AlSb. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 41.7 N/m and 42.0 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer b-AlSb. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -142.4 N/m and -190.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.1 Nm*-1* at the ultimate strain of 0.29 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.1 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CXLII BO
Present studies on the BO are based on first-principles calculations, and no empirical potential has been proposed for the BO. We will thus parametrize a set of SW potential for the single-layer BO in this section.
The structure of the single-layer BO is shown in Fig. 290 with M=B and X=O. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The BO has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior B-B bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 2.44 Å, the bond length Å, and the bond length Å.
Table 566 shows the VFF model for the single-layer BO. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 291 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 291 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 567. The parameters for the three-body SW potential used by GULP are shown in Tab. 568. Parameters for the SW potential used by LAMMPS are listed in Tab. 569.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer BO under uniaxial tension at 1.0 K and 300.0 K. Fig. 292 shows the stress-strain curve for the tension of a single-layer BO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer BO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer BO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 299.6 N/m and 297.7 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer BO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -1554.7 N/m and -1585.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 28.9 Nm*-1* at the ultimate strain of 0.19 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 28.2 Nm*-1* at the ultimate strain of 0.24 in the zigzag direction at the low temperature of 1 K.
CXLIII AlO
Present studies on the AlO are based on first-principles calculations, and no empirical potential has been proposed for the AlO. We will thus parametrize a set of SW potential for the single-layer AlO in this section.
The structure of the single-layer AlO is shown in Fig. 290 with M=Al and X=O. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The AlO has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Al-Al bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 2.96 Å, the bond length Å, and the bond length Å.
Table 570 shows the VFF model for the single-layer AlO. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 293 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 293 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 571. The parameters for the three-body SW potential used by GULP are shown in Tab. 572. Parameters for the SW potential used by LAMMPS are listed in Tab. 573.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer AlO under uniaxial tension at 1.0 K and 300.0 K. Fig. 294 shows the stress-strain curve for the tension of a single-layer AlO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer AlO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer AlO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 149.3 N/m and 148.2 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer AlO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -563.9 N/m and -565.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 19.6 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 20.4 Nm*-1* at the ultimate strain of 0.34 in the zigzag direction at the low temperature of 1 K.
CXLIV GaO
Present studies on the GaO are based on first-principles calculations, and no empirical potential has been proposed for the GaO. We will thus parametrize a set of SW potential for the single-layer GaO in this section.
The structure of the single-layer GaO is shown in Fig. 290 with M=Ga and X=O. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The GaO has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Ga-Ga bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.12 Å, the bond length Å, and the bond length Å.
Table 574 shows the VFF model for the single-layer GaO. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 295 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 295 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 575. The parameters for the three-body SW potential used by GULP are shown in Tab. 576. Parameters for the SW potential used by LAMMPS are listed in Tab. 577.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer GaO under uniaxial tension at 1.0 K and 300.0 K. Fig. 296 shows the stress-strain curve for the tension of a single-layer GaO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer GaO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer GaO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 137.2 N/m and 136.6 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer GaO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -467.5 N/m and -529.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 19.6 Nm*-1* at the ultimate strain of 0.28 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 20.8 Nm*-1* at the ultimate strain of 0.35 in the zigzag direction at the low temperature of 1 K.
CXLV InO
Present studies on the InO are based on first-principles calculations, and no empirical potential has been proposed for the InO. We will thus parametrize a set of SW potential for the single-layer InO in this section.
The structure of the single-layer InO is shown in Fig. 290 with M=In and X=O. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The InO has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior In-In bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.48 Å, the bond length Å, and the bond length Å.
Table 578 shows the VFF model for the single-layer InO. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 297 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 297 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 579. The parameters for the three-body SW potential used by GULP are shown in Tab. 580. Parameters for the SW potential used by LAMMPS are listed in Tab. 581.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer InO under uniaxial tension at 1.0 K and 300.0 K. Fig. 298 shows the stress-strain curve for the tension of a single-layer InO of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer InO is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer InO. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 85.7 N/m along the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer InO. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -157.3 N/m and -210.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 19.9 Nm*-1* at the ultimate strain of 0.38 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 23.6 Nm*-1* at the ultimate strain of 0.39 in the zigzag direction at the low temperature of 1 K.
CXLVI BS
Present studies on the BS are based on first-principles calculations, and no empirical potential has been proposed for the BS. We will thus parametrize a set of SW potential for the single-layer BS in this section.
The structure of the single-layer BS is shown in Fig. 290 with M=B and X=S. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The BS has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior B-B bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.03 Å, the bond length Å, and the bond length Å.
Table 582 shows the VFF model for the single-layer BS. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 299 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 299 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 583. The parameters for the three-body SW potential used by GULP are shown in Tab. 584. Parameters for the SW potential used by LAMMPS are listed in Tab. 585.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer BS under uniaxial tension at 1.0 K and 300.0 K. Fig. 300 shows the stress-strain curve for the tension of a single-layer BS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer BS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer BS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 179.4 N/m and 178.5 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer BS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -793.2 N/m and -823.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 20.0 Nm*-1* at the ultimate strain of 0.21 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 19.5 Nm*-1* at the ultimate strain of 0.28 in the zigzag direction at the low temperature of 1 K.
CXLVII AlS
Present studies on the AlS are based on first-principles calculations, and no empirical potential has been proposed for the AlS. We will thus parametrize a set of SW potential for the single-layer AlS in this section.
The structure of the single-layer AlS is shown in Fig. 290 with M=Al and X=S. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The AlS has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Al-Al bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.57 Å, the bond length Å, and the bond length Å.
Table 586 shows the VFF model for the single-layer AlS. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 301 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 301 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 587. The parameters for the three-body SW potential used by GULP are shown in Tab. 588. Parameters for the SW potential used by LAMMPS are listed in Tab. 589.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer AlS under uniaxial tension at 1.0 K and 300.0 K. Fig. 302 shows the stress-strain curve for the tension of a single-layer AlS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer AlS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer AlS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 85.2 N/m and 84.6 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer AlS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -289.7 N/m and -302.4 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 11.9 Nm*-1* at the ultimate strain of 0.25 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.9 Nm*-1* at the ultimate strain of 0.36 in the zigzag direction at the low temperature of 1 K.
CXLVIII GaS
Present studies on the GaS are based on first-principles calculations, and no empirical potential has been proposed for the GaS. We will thus parametrize a set of SW potential for the single-layer GaS in this section.
The structure of the single-layer GaS is shown in Fig. 290 with M=Ga and X=S. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The GaS has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Ga-Ga bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.64 Å, the bond length Å, and the bond length Å.
Table 590 shows the VFF model for the single-layer GaS. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 303 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 303 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 591. The parameters for the three-body SW potential used by GULP are shown in Tab. 592. Parameters for the SW potential used by LAMMPS are listed in Tab. 593.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer GaS under uniaxial tension at 1.0 K and 300.0 K. Fig. 304 shows the stress-strain curve for the tension of a single-layer GaS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer GaS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer GaS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 76.2 N/m along the armchair and zigzag directions. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer GaS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materigas. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -254.5 N/m and -269.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.0 Nm*-1* at the ultimate strain of 0.36 in the zigzag direction at the low temperature of 1 K.
CXLIX InS
Present studies on the InS are based on first-principles calculations, and no empirical potential has been proposed for the InS. We will thus parametrize a set of SW potential for the single-layer InS in this section.
The structure of the single-layer InS is shown in Fig. 290 with M=In and X=S. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The InS has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior In-In bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.94 Å, the bond length Å, and the bond length Å.
Table 594 shows the VFF model for the single-layer InS. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 305 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 305 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 595. The parameters for the three-body SW potential used by GULP are shown in Tab. 596. Parameters for the SW potential used by LAMMPS are listed in Tab. 597.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer InS under uniaxial tension at 1.0 K and 300.0 K. Fig. 306 shows the stress-strain curve for the tension of a single-layer InS of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer InS is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer InS. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 52.9 N/m and 53.2 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer InS. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -115.9 N/m and -141.1 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.2 Nm*-1* at the ultimate strain of 0.32 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.8 Nm*-1* at the ultimate strain of 0.42 in the zigzag direction at the low temperature of 1 K.
CL BSe
Present studies on the BSe are based on first-principles calculations, and no empirical potential has been proposed for the BSe. We will thus parametrize a set of SW potential for the single-layer BSe in this section.
The structure of the single-layer BSe is shown in Fig. 290 with M=B and X=Se. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The BSe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior B-B bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.25 Å, the bond length Å, and the bond length Å.
Table 598 shows the VFF model for the single-layer BSe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 307 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 307 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 599. The parameters for the three-body SW potential used by GULP are shown in Tab. 600. Parameters for the SW potential used by LAMMPS are listed in Tab. 601.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer BSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 308 shows the stress-strain curve for the tension of a single-layer BSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer BSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer BSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 157.3 N/m and 156.4 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer BSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -627.0 N/m and -655.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 19.2 Nm*-1* at the ultimate strain of 0.23 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 18.7 Nm*-1* at the ultimate strain of 0.31 in the zigzag direction at the low temperature of 1 K.
CLI AlSe
Present studies on the AlSe are based on first-principles calculations, and no empirical potential has been proposed for the AlSe. We will thus parametrize a set of SW potential for the single-layer AlSe in this section.
The structure of the single-layer AlSe is shown in Fig. 290 with M=Al and X=Se. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The AlSe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Al-Al bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.78 Å, the bond length Å, and the bond length Å.
Table 602 shows the VFF model for the single-layer AlSe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 309 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 309 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 603. The parameters for the three-body SW potential used by GULP are shown in Tab. 604. Parameters for the SW potential used by LAMMPS are listed in Tab. 605.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer AlSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 310 shows the stress-strain curve for the tension of a single-layer AlSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer AlSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer AlSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 69.4 N/m and 69.2 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer AlSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -217.3 N/m and -231.9 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.4 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.5 Nm*-1* at the ultimate strain of 0.38 in the zigzag direction at the low temperature of 1 K.
CLII GaSe
Present studies on the GaSe are based on first-principles calculations, and no empirical potential has been proposed for the GaSe. We will thus parametrize a set of SW potential for the single-layer GaSe in this section.
The structure of the single-layer GaSe is shown in Fig. 290 with M=Ga and X=Se. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The GaSe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Ga-Ga bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.82 Å, the bond length Å, and the bond length Å.
Table 606 shows the VFF model for the single-layer GaSe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 311 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 311 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 607. The parameters for the three-body SW potential used by GULP are shown in Tab. 608. Parameters for the SW potential used by LAMMPS are listed in Tab. 609.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer GaSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 312 shows the stress-strain curve for the tension of a single-layer GaSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer GaSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer GaSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 68.3 N/m and 67.9 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer GaSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -206.1 N/m and -219.8 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 10.5 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 10.8 Nm*-1* at the ultimate strain of 0.39 in the zigzag direction at the low temperature of 1 K.
CLIII InSe
Present studies on the InSe are based on first-principles calculations, and no empirical potential has been proposed for the InSe. We will thus parametrize a set of SW potential for the single-layer InSe in this section.
The structure of the single-layer InSe is shown in Fig. 290 with M=In and X=Se. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The InSe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior In-In bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 4.10 Å, the bond length Å, and the bond length Å.
Table 610 shows the VFF model for the single-layer InSe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 313 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 313 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 611. The parameters for the three-body SW potential used by GULP are shown in Tab. 612. Parameters for the SW potential used by LAMMPS are listed in Tab. 613.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer InSe under uniaxial tension at 1.0 K and 300.0 K. Fig. 314 shows the stress-strain curve for the tension of a single-layer InSe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer InSe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer InSe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 45.7 N/m and 45.8 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer InSe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -81.6 N/m and -103.5 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 9.8 Nm*-1* at the ultimate strain of 0.35 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 11.9 Nm*-1* at the ultimate strain of 0.44 in the zigzag direction at the low temperature of 1 K.
CLIV BTe
Present studies on the BTe are based on first-principles calculations, and no empirical potential has been proposed for the BTe. We will thus parametrize a set of SW potential for the single-layer BTe in this section.
The structure of the single-layer BTe is shown in Fig. 290 with M=B and X=Te. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The BTe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior B-B bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 3.56 Å, the bond length Å, and the bond length Å.
Table 614 shows the VFF model for the single-layer BTe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 315 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 315 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 615. The parameters for the three-body SW potential used by GULP are shown in Tab. 616. Parameters for the SW potential used by LAMMPS are listed in Tab. 617.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer BTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 316 shows the stress-strain curve for the tension of a single-layer BTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer BTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer BTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 130.6 N/m and 129.7 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer BTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -560.4 N/m and -588.7 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 14.9 Nm*-1* at the ultimate strain of 0.22 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 14.4 Nm*-1* at the ultimate strain of 0.27 in the zigzag direction at the low temperature of 1 K.
CLV AlTe
Present studies on the AlTe are based on first-principles calculations, and no empirical potential has been proposed for the AlTe. We will thus parametrize a set of SW potential for the single-layer AlTe in this section.
The structure of the single-layer AlTe is shown in Fig. 290 with M=Al and X=Te. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The AlTe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Al-Al bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 4.11 Å, the bond length Å, and the bond length Å.
Table 618 shows the VFF model for the single-layer AlTe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 317 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 317 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 619. The parameters for the three-body SW potential used by GULP are shown in Tab. 620. Parameters for the SW potential used by LAMMPS are listed in Tab. 621.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer AlTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 318 shows the stress-strain curve for the tension of a single-layer AlTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer AlTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer AlTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 55.8 N/m and 54.9 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer AlTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -171.4 N/m and -179.0 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 8.4 Nm*-1* at the ultimate strain of 0.27 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 8.6 Nm*-1* at the ultimate strain of 0.39 in the zigzag direction at the low temperature of 1 K.
CLVI GaTe
Present studies on the GaTe are based on first-principles calculations, and no empirical potential has been proposed for the GaTe. We will thus parametrize a set of SW potential for the single-layer GaTe in this section.
The structure of the single-layer GaTe is shown in Fig. 290 with M=Ga and X=Te. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The GaTe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior Ga-Ga bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 4.13 Å, the bond length Å, and the bond length Å.
Table 622 shows the VFF model for the single-layer GaTe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 319 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 319 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 623. The parameters for the three-body SW potential used by GULP are shown in Tab. 624. Parameters for the SW potential used by LAMMPS are listed in Tab. 625.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer GaTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 320 shows the stress-strain curve for the tension of a single-layer GaTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer GaTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer GaTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 55.2 N/m and 55.3 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer GaTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -183.2 N/m and -195.6 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 7.8 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 7.8 Nm*-1* at the ultimate strain of 0.37 in the zigzag direction at the low temperature of 1 K.
CLVII InTe
Present studies on the InTe are based on first-principles calculations, and no empirical potential has been proposed for the InTe. We will thus parametrize a set of SW potential for the single-layer InTe in this section.
The structure of the single-layer InTe is shown in Fig. 290 with M=In and X=Te. The structural parameters are from the ab initio calculations.Demirci et al. (2017) The InTe has a bi-buckled configuration as shown in Fig. 290 (b), where the buckle is along the zigzag direction. Two buckling layers are symmetrically integrated through the interior In-In bonds, forming a bi-buckled configuration. This structure can be determined by three independent geometrical parameters, eg. the lattice constant 4.40 Å, the bond length Å, and the bond length Å.
Table 626 shows the VFF model for the single-layer InTe. The force constant parameters are determined by fitting to the six low-frequency branches in the phonon dispersion along the M as shown in Fig. 321 (a). The ab initio calculations for the phonon dispersion are from Ref. Demirci et al., 2017. Fig. 321 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 627. The parameters for the three-body SW potential used by GULP are shown in Tab. 628. Parameters for the SW potential used by LAMMPS are listed in Tab. 629.
We use LAMMPS to perform MD simulations for the mechanical behavior of the single-layer InTe under uniaxial tension at 1.0 K and 300.0 K. Fig. 322 shows the stress-strain curve for the tension of a single-layer InTe of dimension Å. Periodic boundary conditions are applied in both armchair and zigzag directions. The single-layer InTe is stretched uniaxially along the armchair or zigzag direction. The stress is calculated without involving the actual thickness of the quasi-two-dimensional structure of the single-layer InTe. The Young’s modulus can be obtained by a linear fitting of the stress-strain relation in the small strain range of [0, 0.01]. The Young’s modulus is 40.6 N/m and 40.9 N/m along the armchair and zigzag directions, respectively. The Poisson’s ratio from the VFF model and the SW potential is .
There is no available value for nonlinear quantities in the single-layer InTe. We have thus used the nonlinear parameter in Eq. (5), which is close to the value of in most materials. The value of the third order nonlinear elasticity can be extracted by fitting the stress-strain relation to the function with as the Young’s modulus. The values of from the present SW potential are -130.4 N/m and -142.2 N/m along the armchair and zigzag directions, respectively. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.26 in the armchair direction at the low temperature of 1 K. The ultimate stress is about 5.9 Nm*-1* at the ultimate strain of 0.38 in the zigzag direction at the low temperature of 1 K.
CLVIII Borophene
Most existing theoretical studies on the monolayer of boron atoms (borophene) are based on the first-principles calculations. The ReaxFF force field model was developed for the borophene recently.Le, Mortazavi, and Rabczuk (2016) The present authors have provided the VFF model and the SW potential to describe the atomic interaction within the borophene,Zhou and Jiang (2017) which includes the second-nearest-neighboring interactions. In the present work, we present a more efficient SW potential with only the first-nearest-neighboring interactions.
The structure of the borophene is shown in Fig. 323, with structural parameters from the ab initio calculations.Wang et al. (2016) Borophene has a puckered configuration as shown in Fig. 323 (b), where the pucker is perpendicular to the x-direction. The height of the pucker is Å, which is the distance between the top chain and the bottom chain along the out-of-plane z-direction. The two lattice bases are Å and Å for the inplane rectangular unit cell. There are two inequivalent boron atoms in the unit cell. Boron atoms are categorized into the top chain and the bottom chain. The top chain includes atoms like 1, 4, and 7. The bottom chain includes atoms like 2, 3, 5, and 6.
Table 630 shows four VFF terms for the borophene, two of which are the bond stretching interaction shown by Eq. (1) while the other two terms are the angle bending interaction shown by Eq. (2). These force constant parameters are determined by fitting to the three acoustic branches in the phonon dispersion along the X as shown in Fig. 324 (a). The ab initio calculations for the phonon dispersion are from Ref. Wang et al., 2016. Similar phonon dispersion can also be found in other ab initio calculations.Pang et al. (2016) Fig. 324 (b) shows that the VFF model and the SW potential give exactly the same phonon dispersion, as the SW potential is derived from the VFF model.
The parameters for the two-body SW potential used by GULP are shown in Tab. 631. The parameters for the three-body SW potential used by GULP are shown in Tab. 632. Parameters for the SW potential used by LAMMPS are listed in Tab. 633. We note that twelve atom types have been introduced for the simulation of borophene using LAMMPS, because the angles around atom 1 in Fig. 323 (a) are not distinguishable in LAMMPS. We thus need to differentiate these angles by assigning these six neighboring atoms (2, 3, 4, 5, 6, 7) with different atom types. Fig. 325 shows that twelve atom types are necessary for the purpose of differentiating all six neighbors around one B atom.
Fig. 326 shows the stress strain relations for the borophene of size Å. The structure is uniaxially stretched in the x or y directions at 1 K and 300 K. The Young’s modulus is 162.7 Nm*-1* and 385.0 Nm*-1* in the x and y directions respectively at 1 K, which are obtained by linear fitting of the stress strain relations in [0, 0.01]. These values are in good agreement with the ab initio results at 0 K temperature, eg. 170 Nm*-1* and 398 Nm*-1* in Ref. Mannix et al., 2015, or 166 Nm*-1* and 389 Nm*-1* in Ref. Wang et al., 2016, or 163 Nm*-1* and 399 Nm*-1* in Ref. Zhang et al., 2017. Previous ab initio calculations obtained negative Poisson’s ratio for the uniaxial stretching of the borophene in the x and y directions, e.g. -0.02 and -0.04 in Refs Mannix et al., 2015 and Wang et al., 2016. The Poisson’s ratio from the present SW potential are -0.03 and -0.07 along the x and y directions respectively, which are quite comparable with the ab initio results.
The third-order nonlinear constant () can be obtained by fitting the stress strain relation to the function , with as the Young’s modulus. The obtained values of are -1100.1 Nm*-1* and -2173.6 Nm*-1* in the x and y directions, respectively. The ultimate stress is about 12.3 Nm*-1* at the critical strain of 0.17 in the x-direction at the low temperature of 1 K, which agree quite well with the ab initio results at 0 K.Wang et al. (2016); Pang et al. (2016); Zhang et al. (2017) The ultimate stress is about 32.9 Nm*-1* at the critical strain of 0.16 in the y-direction at the low temperature of 1 K, which are quite comparable with ab initio results at 0 K.Wang et al. (2016); Pang et al. (2016); Zhang et al. (2017)
CLIX Conclusion Remarks
As a final remark, we note some major advantages and deficiencies for the SW potential parameters provided in the present work. On the one hand, the key feature of the SW potential is its high efficiency, which is maintained by using minimum potential parameters in the present work, so the interaction range is limited to the first-nearest-neighboring atoms. As a result, the present SW potential parameters are of high computational efficiency. On the other hand, since the interaction is limited to short-range, the optical branches in the phonon spectrum are typically overestimated by the present SW potential. It is because we have ignored the long-range interactions, which contribute mostly to the acoustic phonon branches while have neglectable contribution to the optical phonon branches. The short-range interaction has thus been strengthened to give an accurate description for the acoustic phonon branches and the elastic properties, which leads to the overestimation of the optical phonon branches as a trade off. Hence, there will be systematic overestimation for simulating optical processes using the present SW parameters.
We also note that the mathematical form of the SW potential is not suitable for the atomic-thick planar structures, such as graphene and b-BN, because the SW potential are not able to resist the bending motion of these real planar crystals.Arroyo and Belytschko (2004); Jiang et al. (2013)
In conclusion, we have provided the SW potential parameters for 156 layered crystals. The supplemental resources for all simulations in the present work are available online in Ref. Jia, , including a fortran code to generate crystals’ structures, files for molecular dynamics simulations using LAMMPS, files for phonon calculation with the SW potential using GULP, and files for phonon calculations with the valence force field model using GULP.
Acknowledgements The work is supported by the Recruitment Program of Global Youth Experts of China, the National Natural Science Foundation of China (NSFC) under Grant No. 11504225 and the start-up funding from Shanghai University.
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