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Unsteady interactions between shock waves and supersonic turbulent boundary layers are assessed across a variety of conditions. Potentially hazardous fluctuating wall pressures are characterized within a single test facility to establish dominant scaling trends and behaviors.
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This page is a summary of: Unsteady Flow Features Across Different Shock/Boundary-Layer Interaction Configurations, AIAA Journal, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058918.
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