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Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63(sub 1)-012 airfoil section

Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88

Lift and pitching moment at low speeds of the naca 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and double-slotted flap

Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section

Published Year

• 1950-1959 (4)

Subject

• Aerodynamic load (1)
• Airplanes--Models--Testing (1)
• Airplanes--Wings, Swept-back (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Wind tunnel testing (1)

Author

• Kelly, John A. (4) *
• Hayter, Nora-Lee F. (1)

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