Internal flow calculations for axisymmetric supersonic inlets at angle of attack
11th Propulsion Conference ; 1975 ; Anaheim , CA , U.S.A.
01.01.1975
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Internal flow calculations for axisymmetric supersonic inlets at angle of attack
Tema Archiv | 1975
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