Numerical heat conduction in hydrodynamical models of colliding hypersonic flows
E. R. Parkin, J. M. Pittard

TL;DR
This paper investigates how numerical conduction and viscosity affect the dynamics and X-ray emission in hydrodynamical models of colliding hypersonic flows, emphasizing the importance of resolution and numerical effects.
Contribution
It systematically analyzes the impact of numerical conduction and viscosity on simulated shock dynamics and emission, providing insights for more accurate astrophysical modeling.
Findings
Numerical conduction causes erroneous heating across contact discontinuities.
Increased numerical viscosity dampens instabilities and can re-heat gas via sub-shocks.
Higher resolution reduces numerical conduction effects.
Abstract
Hydrodynamical models of colliding hypersonic flows are presented which explore the dependence of the resulting dynamics and the characteristics of the derived X-ray emission on numerical conduction and viscosity. For the purpose of our investigation we present models of colliding flow with plane-parallel and cylindrical divergence. Numerical conduction causes erroneous heating of gas across the contact discontinuity which has implications for the rate at which the gas cools. We find that the dynamics of the shocked gas and the resulting X-ray emission are strongly dependent on the contrast in the density and temperature either side of the contact discontinuity, these effects being strongest where the postshock gas of one flow behaves quasi-adiabatically while the postshock gas of the other flow is strongly radiative. Introducing additional numerical viscosity into the simulations has…
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