Experimental investigation of hypersonic boundary layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2011
|MEASUREMENT OF HYPERSONIC HIGH-ENTHALPY BOUNDARY LAYER TRANSITION ON 7^o CONE MODEL
British Library Conference Proceedings | 2010
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