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 ; San Francisco, CA
2011-01-01
9 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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MEASUREMENT OF HYPERSONIC HIGH-ENTHALPY BOUNDARY LAYER TRANSITION ON 7^o CONE MODEL
British Library Conference Proceedings | 2010
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