A study of the flow structure for Mach reflection in steady supersonic flow
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Publication:3053570
DOI10.1017/S0022112010001011zbMath1197.76076MaRDI QIDQ3053570
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Publication date: 29 October 2010
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Related Items (14)
Reflection and transition of planar curved shock waves ⋮ Time history of regular to Mach reflection transition in steady supersonic flow ⋮ Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges ⋮ Steady Mach reflection with two incident shock waves ⋮ Application of the minimum entropy production principle to shock reflection induced by separation ⋮ Prediction of Mach stem height in compressible open jets. Part 1. Overexpanded jets ⋮ A study of the asymmetric shock reflection configurations in steady flows ⋮ Size and shape of shock waves and slipline for Mach reflection in steady flow ⋮ Mach reflection promoted by an upstream shock wave ⋮ An analytical model for asymmetric Mach reflection configuration in steady flows ⋮ Study of asymmetrical shock wave reflection in steady supersonic flow ⋮ E-H type Mach configuration and its stability ⋮ Double solution and influence of secondary waves on transition criteria for shock interference in pre-Mach reflection with two incident shock waves ⋮ Shock reflection in the presence of an upstream expansion wave and a downstream shock wave
Cites Work
- Shock wave reflection phenomena
- Modification of Whitham's ray shock theory for analyzing the reflection of weak shock waves over small wedge angles
- A robust shock-capturing scheme based on rotated Riemann solvers.
- Engineering approach to the prediction of shock patterns in bounded high-speed flows
- A parametric study of Mach reflection in steady flows
- Hysteresis effect in stationary reflection of shock waves
- On initial-value and self-similar solutions of the compressible Euler equations
- Flow-Mach-number-induced hysteresis phenomena in the interaction of conical shock waves – a numerical investigation
- Determination of the sonic line in hypersonic flow past a blunt body
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