Analysis and Design of a Hypersonic Scramjet Engine with a Transition Mach Number of 4.00
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; 2009 ; Orlando , Florida
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Analysis and Design of a Hypersonic Scramjet Engine with a Transition Mach Number of 4.00
British Library Conference Proceedings | 2009
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