Time history of regular to Mach reflection transition in steady supersonic flow

DOI10.1017/JFM.2011.201zbMath1241.76316OpenAlexW2327104928MaRDI QIDQ2891833

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Publication date: 15 June 2012

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2011.201

zbMATH Keywords

shock wavesgas dynamicshigh-speed flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Related Items (6)

Reflection and transition of planar curved shock waves ⋮ Steady Mach reflection with two incident shock waves ⋮ Prediction of Mach stem height in compressible open jets. Part 1. Overexpanded jets ⋮ Shock transformation and hysteresis in underexpanded confined jets ⋮ Transition study for asymmetric reflection between moving incident shock waves ⋮ Shock reflection in the presence of an upstream expansion wave and a downstream shock wave

Cites Work

• Shock wave reflection phenomena
• Assessment of Riemann solvers for unsteady one-dimensional inviscid flows of perfect gases
• A robust shock-capturing scheme based on rotated Riemann solvers.
• Numerical investigations of transition between regular and Mach reflections caused by free-stream disturbances
• A study of the flow structure for Mach reflection in steady supersonic flow

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