Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-off Distance
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
2009-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-Off Distance
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