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High-speed schlieren imaging was used to examine a shock wave boundary layer (SBLI) as the state of the interaction was brought through transition. Key findings included the outboard motion of separation shocks and high-frequency content within the interaction.
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This page is a summary of: High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions, AIAA Journal, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059193.
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