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
|Boundary-layer development and skin friction at Mach number 3.05
TIBKAT | 1952
|