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A wedge is free to pitch in a Mach 6 flow. The wedge creates an oscillating shock which impinges on a plate beneath the wedge. This work is about the study of the interaction between the moving shock and the boundary layer on the plate
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This page is a summary of: Hypersonic Oscillating Shock-Wave/Boundary-Layer Interaction on a Flat Plate, AIAA Journal, March 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059590.
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