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
01.01.1962
Sonstige
Keine Angabe
Englisch
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
|