Force and pressure tests of the GA(W)-1 airfoil with a 20% aileron and pressure tests with a 30% Fowler flap
W. H. Wentz, H. C. Seetharam, K. A. Fiscko
Abstract
W. H. Wentz, H. C. Seetharam, K. A. Fiscko
Abstract
Prepared by Wichita State University under contract no. NSG-1165, for Langley Research Center.;Issued June 1977.
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Prepared by Wichita State University under contract no. NSG-1165, for Langley Research Center.;Issued June 1977.
Key concepts: Aileron, Airfoil, Camber (aerodynamics), Structural engineering, Angle of attack, Hinge, Deflection (physics), Aeroelasticity