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Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=cCfw5d8xFjQC&hl=&source=gbs_api
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