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Effects at Mach Numbers of 1.61 and 2.01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform
Emma Jean Landrum
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=vgEOEYeb_2UC&hl=&source=gbs_api
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