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Hypersonic boundary layer transition is one of important problems in the engineering design of hypersonic aircraft. We develop a new numerical model to prediticting boundary layer transition behavior in hypersonic flows.

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This page is a summary of: Improved Transition Model with Mechanical Considerations for Hypersonic Flow, AIAA Journal, October 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061817.
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