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Maximum Lift and Longitudinal Stability Characteristics at Reynolds Numbers Up to 7.8 X (10)6 of a 35 Degrees Sweptforward Wing Equipped with High-lift and Stall-control Devices, Fuselage and Horizontal Tail

Albert P. Martina

出版	NACA, 1950
URL	http://books.google.com.hk/books?id=ruEByAEACAAJ&hl=&source=gbs_api