Prediction of flow angularity near a supersonic fuselage forebody with arbitrary cross-section
8th Annual Meeting and Technical Display ; 1971 ; Washington , DC , U.S.A.
1971-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Computational investigation of slot blowing for fuselage forebody flow control
Online Contents | 1999
|Forebody effects on drogue drag in supersonic flow.
AIAA | 1968
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