Irregular effects on the transition from regular to Mach reflection of shock waves in wind tunnel flows

DOI10.1017/S0022112002007966zbMath0991.76511OpenAlexW1987635540MaRDI QIDQ4542391

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Publication date: 8 September 2002

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

Full work available at URL: https://doi.org/10.1017/s0022112002007966

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05)

Related Items (12)

Dynamic effects on the transition between two-dimensional regular and Mach reflection of shock waves in an ideal, steady supersonic free stream ⋮ Experiments on the mechanism of inducing transition between regular and Mach reflection ⋮ Geometric criterion for RR↔MR transition in hypersonic double-wedge flows ⋮ Three-dimensional shock wave reflection transition in steady flow ⋮ On the RR \(\to\) MR transition of asymmetric shock waves in steady flows ⋮ Shock transformation and hysteresis in underexpanded confined jets ⋮ Effects of a single-pulse energy deposition on steady shock wave reflection ⋮ Mach reflection promoted by an upstream shock wave ⋮ Study of asymmetrical shock wave reflection in steady supersonic flow ⋮ Shock reflection and oblique shock waves ⋮ Downstream flow condition effects on the RR → MR transition of asymmetric shock waves in steady flows ⋮ Dynamics of unsteady asymmetric shock interactions

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