Numerical and Experimental Investigation on Detonation Tube for Simulating the Rocket Exhaust Gas at High Enthalpy Shock Tunnel
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2009
|Detonation tube technique for simulating rocket plumes in space environment
Engineering Index Backfile | 1968
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