Influence of numerical and viscous dissipation on shock wave reflections in supersonic steady flows.
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Publication:1871594
DOI10.1016/S0045-7930(02)00002-6zbMath1084.76535MaRDI QIDQ1871594
Marie-Claude Druguet, David E. Zeitoun
Publication date: 4 May 2003
Published in: Computers and Fluids (Search for Journal in Brave)
Mach reflectionRegular reflection\(H\)-correctionFinite volumes methodMach stem and triple point configurationRoe flux splitting
Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12) Supersonic flows (76J20)
Related Items (2)
Aerodynamic response of internal passages to pulsating inlet supersonic conditions ⋮ Healing of shock instability for Roe's flux-difference splitting scheme on triangular meshes
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Cites Work
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- Engineering approach to the prediction of shock patterns in bounded high-speed flows
- A parametric study of Mach reflection in steady flows
- Dependence of Steady Mach Reflections on the Reflecting-Wedge Trailing-Edge Angle
- Numerical instabilities in upwind methods: Analysis and cures for the ``carbuncle phenomenon
- Steady shock wave reflections in thermochemical nonequilibrium flows
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