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
British Library Conference Proceedings | 2013
|Wall Pressure Fluctuations in a Turbulent Boundary Layer
NTRS | 1958
|A High Mach Number Turbulent Boundary-Layer Study
AIAA | 1976
|