Research on the Influence of Fluidic Thrust Vector Parameters on the Single Expansion Ramp Nozzle of the Air-breathing Hypersonic Vehicle (AIAA 2017-2113)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
2017-01-01
8 pages
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 2005
|Hypersonic single expansion ramp nozzle simulations
NTRS | 1992
|Hypersonic single expansion ramp nozzle simulations
AIAA | 1992
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