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Test of NACA 66,2-116, a =0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

Wind tunnel investigation of control surface characteristics.12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance

Published Year

• 1940-1949 (2) *

Subject

• Charts, diagrams, etc (2)
• Hinge moments (Aerodynamics) (2) *
• Wind tunnel testing (2)
• Aerodynamic load (1)
• Aerofoils (1)
• Aerofoils--Testing (1)
• Airplanes--Control surfaces (1)
• Drag (Aerodynamics) (1)
• Flaps (Aerodynamics) (1)
• Flaps (Airplanes) (1)
• Lift (Aerodynamics) (1)
• Plates (Engineering) (1)

Author

• Abbott, Frank T. (1)
• Hoggard, H. Page. (1)
• Underwood, William J. (1)

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