Enhanced approximate Riemann solvers for all-Mach number flows using anti-diffusion coefficients

This paper compares the Harten–Lax–Leer–Einfeldt Modified (HLLEM) and Harten–Lax–Leer Convective Pressure Split (HLL-CPS) schemes for Euler equations and proposes improvements for all-Mach number flows. Enhancements to the HLLEM scheme involve adding anti-diffusion terms in the face normal direction and modifying anti-diffusion coefficients for linearly degenerate waves near shocks. The HLL-CPS scheme is improved by adjusting anti-diffusion coefficients for the face normal direction and linearly degenerate waves. Matrix stability, linear perturbation, and asymptotic analyses demonstrate the robustness of the proposed schemes and their ability to capture low Mach flow features. Numerical tests confirm that the schemes are free from shock instabilities at high speeds and accurately resolve low Mach number flow features.

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Publication Details

Journal
Physics of Fluids
Published
2025-02-01
DOI
https://doi.org/10.1063/5.0248756
Citations
1
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
1.33
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article

Enhanced approximate Riemann solvers for all-Mach number flows using anti-diffusion coefficients

J. C. Mandal, A. Gogoi
1 citations
Physics of Fluids
Computational Fluid Dynamics and Aerodynamics
1.33
article

Enhanced approximate Riemann solvers for all-Mach number flows using anti-diffusion coefficients

J. C. Mandal, A. Gogoi
article en
1 citations

Abstract

This paper compares the Harten–Lax–Leer–Einfeldt Modified (HLLEM) and Harten–Lax–Leer Convective Pressure Split (HLL-CPS) schemes for Euler equations and proposes improvements for all-Mach number flows. Enhancements to the HLLEM scheme involve adding anti-diffusion terms in the face normal direction and modifying anti-diffusion coefficients for linearly degenerate waves near shocks. The HLL-CPS scheme is improved by adjusting anti-diffusion coefficients for the face normal direction and linearly degenerate waves. Matrix stability, linear perturbation, and asymptotic analyses demonstrate the robustness of the proposed schemes and their ability to capture low Mach flow features. Numerical tests confirm that the schemes are free from shock instabilities at high speeds and accurately resolve low Mach number flow features.

Physics of FluidsVol. 37(2)
Aeronautical Development Agency (IN), Indian Institute of Technology Bombay (IN)
Openalex Percentile: Top 26%
Computational Fluid Dynamics and Aerodynamics
1.33
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Enhanced approximate Riemann solvers for all-Mach number flows using anti-diffusion coefficients — J. C. Mandal, A. Gogoi · Physics of Fluids (2025) | TGRS Research Map | TGRS