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Wing-on and Wing-off Longitudinal Characteristics of an Airplane Configuration Having a Thin Unswept Tapered Wing of Aspect Ratio 3, as Obtained from Rocket-propelled Models at Mach Numbers from 0.8 to 1.4

出版	NACA, 1951
URL	http://books.google.com.hk/books?id=vNsryAEACAAJ&hl=&source=gbs_api