Finite wing lift prediction at high angles of attack
Flight Simulation Technologies Conference and Exhibit ; 1990 ; Dayton , OH , U.S.A.
01.01.1990
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
|Spanwise Distribution of Lift and Drag at High Angles of Attack
SAE Technical Papers | 1989
|