Effects of yaw on leading edge vortex flap aerodynamics
Aircraft Systems and Technology Conference ; 1981 ; Dayton , OH , U.S.A.
01.01.1981
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
High-Incidence Airfoil Aerodynamics Improvement by Leading-Edge Oscillating Flap
Online Contents | 1998
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