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Experiments Giving Hinge Moment and Lift on a NACA 0015 Aerofoil Fitted with a 40 Per Cent Control, with Especial Reference to Effect of Curvature of Control Surface

Aeronautical Research Council (Great Britain)Alan Stewart BatsonJ. H. PrestonJ. H. Warsap

出版	H.M. Stationery Office, 1952
URL	http://books.google.com.hk/books?id=zamvDAEACAAJ&hl=&source=gbs_api