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Aerodynamic Characteristics in Pitch of a Series of Cruciform-wing Missiles with Canard Controls at a Mach Number of 2.01
M. Leroy Spearman
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=hDuO_EWzHnoC&hl=&source=gbs_api
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