A computational study of incipient leading-edge separation on a 65-deg delta wing at M = 1.60
Flight Simulation Technologies Conference and Exhibit ; 1990 ; Dayton , OH , U.S.A.
01.01.1990
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Control of Leading-Edge Separation on a Cambered Delta Wing
British Library Conference Proceedings | 1994
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