Transition on swept leading edges at Mach 3.5
Journal of Aircraft ; 24
1987-10-01
Miscellaneous
No indication
English
Transition on swept leading edges at Mach 3.5
AIAA | 1987
|On the flow along swept leading edges
TIBKAT | 1965
|Relaminarization on swept leading edges under high-lift conditions
Tema Archive | 2006
|