Effects of fin leading edge sweep on shock-shock interaction at Mach 6
34th Aerospace Sciences Meeting and Exhibit ; 1996 ; Reno , NV , U.S.A.
01.01.1996
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Fin Leading-Edge Sweep Effect on Shock-Shock Interaction at Mach 6
Online Contents | 1997
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