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Effects of Angle of Attack and Thickness Ratio on the Flutter of a Rigid Unswept Diamond-airfoil-section Wing at a Mach Number of 10.0
Lou S. Young
出版National Aeronautics and Space Administration, 1962
URLhttp://books.google.com.hk/books?id=oecSyFIvnmoC&hl=&source=gbs_api
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