Effect of Mach number on boundary layer noise
20th AIAA/CEAS Aeroacoustics Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A High Mach Number Turbulent Boundary-Layer Study
AIAA | 1976
|Shock-Wave/Boundary-Layer Interactions in High-Mach-Number Flows
British Library Online Contents | 1996
|