Comparative flow path analysis and design assessment of an axisymmetric hydrogen fueled scramjet flight test engine at a Mach number of 6.5
Space Plane and Hypersonic Systems and Technology Conference ; 1996 ; Norfolk , VA , U.S.A.
01.01.1996
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 1996
|British Library Conference Proceedings | 1996
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