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
2011-01-01
Conference paper
Electronic Resource
English
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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