STABILITY LIMIT OF SUPERMULTI-JETS CONVERGENCE ENGINE OPERATED FROM STARTUP TO EXTREMELY-HYPERSONIC CONDITIONS: REVEALED BY SHOCK-TUBE EXPERIMENTS
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
2012-01-01
10 pages
Includes bibliographical references and index
Conference paper
English
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