Direct numerical simulation of hypersonic turbulent boundary layers with varying freestream Mach number
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
DNS OF HYPERSONIC TURBULENT BOUNDARY LAYERS VARYING FREESTREAM MACH NUMBER
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|Receptivity of Hypersonic Boundary Layers to Freestream Disturbances
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