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
Sonstige
Keine Angabe
Englisch
Study on Non-Equilibrium Flow Behind Hypersonic Shock Waves of About Mach 10
British Library Conference Proceedings | 1999
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