Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10
7th AIAA Theoretical Fluid Mechanics Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10
British Library Conference Proceedings | 2014
|Boundary layer transition at hypersonic Mach numbers.
NTRS | 1967
|