Boundary-Layer Transition Induced by an Isolated Roughness Element in Mach 6 Quiet Flow
AIAA SCITECH 2024 Forum
2024-01-01
Conference paper
Electronic Resource
English
Compressibility Effects on Boundary-Layer Transition Induced by an Isolated Roughness Element
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|HYPERSONIC BOUNDARY-LAYER TRANSITION EXPERIMENTS IN A MACH-6 QUIET TUNNEL
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