A new coupled computational method in conjunction with three-dimensional finite volume schemes for nonlinear coupled constitutive relations
Zhongzheng Jiang, Weifang Chen, Wenwen Zhao

TL;DR
This paper evaluates a modified nonlinear coupled constitutive relations (NCCR) model using advanced finite volume schemes for three-dimensional hypersonic rarefied gas flows, demonstrating improved accuracy over traditional NSF equations.
Contribution
It introduces a modified NCCR computational approach with finite volume schemes for 3D complex flows, enhancing stability and accuracy in hypersonic rarefied gas simulations.
Findings
Modified NCCR yields results closer to DSMC and experimental data.
Finite volume schemes effectively solve 3D hypersonic rarefied flows.
The approach shows promise for practical high-speed flow applications.
Abstract
Non-equilibrium effects play a vital role in high-speed and rarefied gas flows and the accurate simulation of these flow regimes are far beyond the capability of near-local-equilibrium Navier-Stokes-Fourier equations. Eu proposed generalized hydrodynamic equations which are consistent with the laws of irreversible thermodynamics to solve this problem. Based on Eu's generalized hydrodynamics equations, a computational model, namely the nonlinear coupled constitutive relations(NCCR),was developed by R.S.Myong and applied successfully to one-dimensional shock wave structure and two-dimensional rarefied flows. In this paper, finite volume schemes, including LU-SGS time advance scheme, MUSCL interpolation and AUSMPW+ scheme, are fistly adopted to investigate NCCR model's validity and potential in three-dimensional complex hypersonic rarefied gas flows. Moreover, in order to solve the…
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Taxonomy
TopicsGas Dynamics and Kinetic Theory · Computational Fluid Dynamics and Aerodynamics · Plasma and Flow Control in Aerodynamics
