Numerical Simulation of a Shock Wave Interaction with an Anisotropic Entropy Perturbation Field

The paper investigates the interaction between a shock wave and an anisotropic entropy perturbation field. An analytical solution is derived for the pressure perturbation behind the shock front, including second-order corrections. Using the example of two colliding plates, the problem of shock wave propagation in an impactor with initial density perturbations is solved numerically. A comparison between the analytical estimates and numerical simulations results is presented. The obtained solution can be used for verification during the development of new numerical schemes.

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Publication Details

Journal
Mathematical Models and Computer Simulations
Published
2025-12-01
DOI
https://doi.org/10.1134/s2070048225700632
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
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article

Numerical Simulation of a Shock Wave Interaction with an Anisotropic Entropy Perturbation Field

K. E. Gorodnichev, E. M. Urvachev, S. E. Kuratov
Mathematical Models and Computer Simulations
Computational Fluid Dynamics and Aerodynamics
article

Numerical Simulation of a Shock Wave Interaction with an Anisotropic Entropy Perturbation Field

K. E. Gorodnichev, E. M. Urvachev, S. E. Kuratov
article en

Abstract

The paper investigates the interaction between a shock wave and an anisotropic entropy perturbation field. An analytical solution is derived for the pressure perturbation behind the shock front, including second-order corrections. Using the example of two colliding plates, the problem of shock wave propagation in an impactor with initial density perturbations is solved numerically. A comparison between the analytical estimates and numerical simulations results is presented. The obtained solution can be used for verification during the development of new numerical schemes.

Mathematical Models and Computer SimulationsVol. 17(S1)
All Russia Research Institute of Automatics (RU), Keldysh Institute of Applied Mathematics (RU)
Openalex Percentile: Top 30%
Computational Fluid Dynamics and Aerodynamics
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