Title: Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section
Abstract: Report presenting an investigation in the two-dimensional low-turbulence tunnel to develop flap configurations for maximum lift of the NACA 65-210 airfoil section equipped with four types of high-lift flap. Lift and pitching-moment data were obtained for the optimum configurations. Results regarding the optimum configurations for maximum lift, scale effect, effect of roughness, pitching moments, and comparison of flaps are provided.
Publication Year: 1947
Publication Date: 1947-02-01
Language: en
Type: article
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Cited By Count: 1
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