Numerical Study of Pressure Fluctuations due to a Mach 6 Turbulent Boundary Layer
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Study of Pressure Fluctuations due to a Mach 6 Turbulent Boundary Layer
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