Boundary layers in axisymmetric inlets at angle of attack. I - Measurements
14th Joint Propulsion Conference ; 1978 ; Las Vegas , NV , U.S.A.
01.01.1978
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Internal flow calculations for axisymmetric supersonic inlets at angle of attack
Tema Archiv | 1975
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