Downstream flow condition effects on the RR → MR transition of asymmetric shock waves in steady flows
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Publication:3616196
DOI10.1017/S0022112008004837zbMath1156.76411OpenAlexW2167058457MaRDI QIDQ3616196
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Publication date: 24 March 2009
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/s0022112008004837
Related Items (8)
Computational confirmation of an abnormal Mach reflection wave configuration ⋮ On the numerical technique for the simulation of hypervelocity test flows ⋮ Geometric criterion for RR↔MR transition in hypersonic double-wedge flows ⋮ Application of the minimum entropy production principle to shock reflection induced by separation ⋮ Shock transformation and hysteresis in underexpanded confined jets ⋮ Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a \(M_\infty=9\) hypersonic flow ⋮ On the modified dispersion-controlled dissipative (DCD) scheme for computation of flow supercavitation ⋮ Transitions of shock interactions on V-shaped blunt leading edges
Cites Work
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- A state-of-the-knowledge review on pseudo-steady shock-wave reflections and their transition criteria
- Self-induced oscillations in the shock wave flow pattern formed in a stationary supersonic flow over a double wedge
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- Numerical study of inviscid shock interactions on double-wedge geometries
- Three-dimensional effects in wind tunnel studies of shock wave reflection
- Irregular effects on the transition from regular to Mach reflection of shock waves in wind tunnel flows
- Analytical and experimental investigations of the reflection of asymmetric shock waves in steady flows
- Transition between regular and Mach reflection of shock waves: New numerical and experimental results
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