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Experimental characterization of shock wave/transitional boundary layer interactions using schlieren imaging focusing on the boundary layer separation between the upstream influence shock and the separation shock.
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This page is a summary of: Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8, AIAA Journal, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059980.
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