Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnel
AIAA Aircraft Design and Operations Meeting ; 1969 ; Los Angeles , California
1969-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
INVESTIGATION OF SUPERSONIC COMBUSTION THROUGH MODEL SCRAMJET ENGINE DESIGN AND SHOCK TUNNEL TESTS
British Library Conference Proceedings | 2009
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