Title: 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
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.
Publication Year: 1953
Publication Date: 1953-09-01
Language: en
Type: article
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Cited By Count: 8
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