Size and shape of shock waves and slipline for Mach reflection in steady flow

DOI10.1017/jfm.2017.139zbMath1383.76396OpenAlexW2600294403MaRDI QIDQ5364650

Chen-Yuan Bai, Zi-Niu Wu

Publication date: 28 September 2017

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

Full work available at URL: https://doi.org/10.1017/jfm.2017.139

zbMATH Keywords

shock wavesgas dynamicshigh-speed flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Gas dynamics (general theory) (76N15)

Related Items (11)

Reflection and transition of planar curved shock waves ⋮ 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 ⋮ 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 ⋮ Mach stem deformation in pseudo-steady shock wave reflections ⋮ Double solution and influence of secondary waves on transition criteria for shock interference in pre-Mach reflection with two incident shock waves ⋮ Transitions of shock interactions on V-shaped blunt leading edges

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• Oblique-shock/expansion-fan interaction - Analytical solution
• Experiments on the mechanism of inducing transition between regular and Mach reflection
• Interaction of a Simple Expansion Wave with a Shock Wave in Two-Dimensional Flows of a Gas
• Analytical and numerical study of the near flow field and shape of the Mach stem in steady flows

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