Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a \(M_\infty=9\) hypersonic flow

DOI10.1007/S00162-010-0188-4zbMath1234.76035OpenAlexW1984311225MaRDI QIDQ407776

J. Herrera, H. S. Yoon

Publication date: 27 March 2012

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00162-010-0188-4

zbMATH Keywords

hysteresisoscillationhypersonicdouble wedgeshock/shock interaction

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Cites Work

• Numerical confirmation of the hysteresis phenomenon in the regular to the Mach reflection transition in steady flows
• Shock dynamics
• Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
• Self-induced oscillations in the shock wave flow pattern formed in a stationary supersonic flow over a double wedge
• Downstream flow condition effects on the RR → MR transition of asymmetric shock waves in steady flows
• Triple-shock entropy theorem and its consequences
• Numerical study of inviscid shock interactions on double-wedge geometries
• Analytical and experimental investigations of the reflection of asymmetric shock waves in steady flows
• Computational confirmation of an abnormal Mach reflection wave configuration
• CRITICAL HYPERSONIC AEROTHERMODYNAMIC PHENOMENA
• Transition between regular and Mach reflection of shock waves: New numerical and experimental results

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