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Hypersonic boundary-layer transition significantly affects the performance of a hypersonic vehicle. We investigated the effects of local and full wall cooling on boundary layer stability.
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This page is a summary of: Local Wall Cooling Effects on Hypersonic Boundary-Layer Stability, Journal of Spacecraft and Rockets, October 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35404.
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