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Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8
出版National Aeronautics and Space Administration, 1960
URLhttp://books.google.com.hk/books?id=Ckx9_yYFP94C&hl=&source=gbs_api
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