Influence of numerical and viscous dissipation on shock wave reflections in supersonic steady flows.

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)

zbMATH Keywords

Mach reflectionRegular reflection\(H\)-correctionFinite volumes methodMach stem and triple point configurationRoe flux splitting

Mathematics Subject Classification ID

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

Uses Software

• HE-E1GODF

Cites Work

• Unnamed Item
• Shock wave reflection phenomena
• Multidimensional dissipation for upwind schemes: Stability and applications to gas dynamics
• Analytical prediction of the wave configuration size in steady flow Mach reflections
• Investigation of the hysteresis phenomena in steady shock reflection using kinetic and continuum methods
• Stability of shock wave reflections in nonequilibrium steady flows and hysteresis
• 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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