Experiments on a 3D expansion-compression cone at Mach 5-8 show that increasing Reynolds number shrinks the separation bubble while Mach-8 relaminarization prevents fully turbulent interaction and alters flapping and breathing motions.
Supersonic Separated and Reattaching Laminar Flows: I. General Theory and Application to Adiabatic Boundary-Layer/Shock-Wave Interactions,
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Hypersonic Shock-Wave/Boundary-Layer Interaction on a Three-Dimensional Expansion-Compression Geometry
Experiments on a 3D expansion-compression cone at Mach 5-8 show that increasing Reynolds number shrinks the separation bubble while Mach-8 relaminarization prevents fully turbulent interaction and alters flapping and breathing motions.