Engine inlet distortion in a 9.2 percent scaled vectored thrust STOVL model in ground effect
25th Joint Propulsion Conference ; 1989 ; Monterey , CA , U.S.A.
01.01.1989
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
The Synthesis of Ejector Lift/Vectored Thrust for STOVL
SAE Technical Papers | 1987
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