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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

Nora-Lee F Hayter, John A Kelly

Abstract

Report presenting a two-dimensional wind-tunnel investigation at low speeds of the NACA 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and a double-slotted flap. Optimum slat positions and section lift and pitching moment characteristics of the model arrangements were determined for various Reynolds numbers.

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Available abstract

Key concepts: Airfoil, Lift (data mining), Wind tunnel, Pitching moment, Leading edge, Reynolds number, NACA airfoil, Section (typography)