Experimental and Numerical Investigations of a Scramjet Model Tested in the H2K Blow Down Wind Tunnel at Mach 7 Flight Condition (AIAA 2014-2933)
19th, AIAA international space planes and hypersonic systems and technologies conference ; 2014 ; Atlanta, GA
2014-01-01
14 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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