Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
INFLUENCE OF FAVORABLE PRESSURE GRADIENTS ON A MACH 5.0 TURBULENT BOUNDARY LAYER
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