Finite wing lift prediction at high angles of attack
Flight Simulation Technologies Conference and Exhibit ; 1990 ; Dayton , OH , U.S.A.
1990-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Active control of vortex lift at high angles of attack
AIAA | 1995
|Calculation of Wing-Alone Aerodynamics to High Angles of Attack
Online Contents | 1995
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