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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

Published Year

• 1940-1949 (1)

Subject

• Aerodynamic load (1)
• Aerofoils--Testing (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Flaps (Aerodynamics) (1)
• Hinge moments (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Wind tunnel testing (1) *

Author

• Abbott, Frank T. (1)
• Underwood, William J. (1) *

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