Attachment line transition studies on swept cylindrical leading edges at Mach numbers from 10 to 12
Fluid Dynamics Conference ; 1995 ; San Diego , CA , U.S.A.
01.01.1995
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Transition on swept leading edges at Mach 3.5
NTRS | 1987
|Transition on swept leading edges at Mach 3.5
AIAA | 1987
|Engineering Index Backfile | 1959
|