Mass injection effects on viscous hypersonic low Reynolds number shock layer downstream and at stagnation point in blunt forebody region analyzed for nonreacting gas
Hypersonic, low-Reynolds-number flow over a blunt body with mass injection.
01.08.1969
Sonstige
Keine Angabe
Englisch
Hypersonic Flow over a Blunt Body with Plasma Injection
British Library Conference Proceedings | 2001
|Hypersonic Flow over a Blunt Body with Plasma Injection
AIAA | 2002
|Hypersonic flow over a blunt body with plasma injection
AIAA | 2001
|