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Experimental and numerical data were used to derive semi-empirical formulas for transition prediction in a swept-wing boundary layer for a range of subsonic flow velocities and different roughness configurations.
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This page is a summary of: Description and Prediction of Roughness-Induced Transition in Swept-Wing Boundary Layers, AIAA Journal, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064370.
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