Boundary-Layer Separation Due to Combustion-Induced Pressure Rise in a Supersonic Flow
AIAA Journal ; 47 , 4 ; 1050-1053
2009-04-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Boundary layer separation in two-dimensional supersonic flow
TIBKAT | 1956
|Supersonic, Turbulent Boundary-Layer Separation
AIAA | 1974
|Boundary-Layer Code For Supersonic Combustion
NTRS | 1994
|