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Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75°
Gerald V. Foster
出版National Aeronautics and Space Administration, 1960
URLhttp://books.google.com.hk/books?id=mq1fLNnuf1YC&hl=&source=gbs_api
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