Hypersonic approximation of the minimum semiapex angle giving subsonic flow behind an attached shock
HYPERSONIC APPROXIMATION OF THE MINIMUM SEMIAPEX ANGLE GIVING SUBSONIC FLOW BEHIND AN ATTACHED SHOCK
1962-01-01
Miscellaneous
No indication
English
On flow behind attached curved shock
Engineering Index Backfile | 1952
|Study on Non-Equilibrium Flow Behind Hypersonic Shock Waves of About Mach 10
British Library Conference Proceedings | 1999
|