Boundary-Layer Transition Induced by an Isolated Roughness Element in Mach 6 Quiet Flow
AIAA SCITECH 2024 Forum
2024-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
HYPERSONIC BOUNDARY-LAYER TRANSITION EXPERIMENTS IN A MACH-6 QUIET TUNNEL
British Library Conference Proceedings | 2010
|Compressibility Effects on Boundary-Layer Transition Induced by an Isolated Roughness Element
Online Contents | 2010
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