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A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=XVRYzT3Te3oC&hl=&source=gbs_api
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