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Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
出版National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979
URLhttp://books.google.com.hk/books?id=w-MQAQAAIAAJ&hl=&source=gbs_api
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