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This paper discusses the transition prediction for hypersonic boundary layers in the presence of wall mass injection, and indicates a promising direction towards pushing wall mass injection into applications of transition model.

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This page is a summary of: Local-Variable-Based Transition Model for Hypersonic Flows Considering Wall Mass Injection, AIAA Journal, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064279.
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