Viscous simulation of shock-reflection hysteresis in overexpanded planar nozzles
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Publication:3550367
DOI10.1017/S002211200900771XzbMath1183.76795OpenAlexW2007731572MaRDI QIDQ3550367
Avi Levy, E. Shimshi, Gabi Ben-Dor
Publication date: 31 March 2010
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/s002211200900771x
Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12)
Related Items (2)
Prediction of Mach stem height in compressible open jets. Part 1. Overexpanded jets ⋮ Shock transformation and hysteresis in underexpanded confined jets
Cites Work
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- Analysis of an RNG based turbulence model for separated flows
- Analytical prediction of the wave configuration size in steady flow Mach reflections
- Differential characteristics of the flow field in a plane overexpanded jet in the vicinity of the nozzle lip
- A parametric study of Mach reflection in steady flows
- Transition between regular and Mach reflection of shock waves: New numerical and experimental results
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