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Performance of a Translating-double-cone Axisymmetric Inlet with Cowl Bypass at Mach Number from 2.0 to 3.5
James F. ConnorsGeorgeA. Wise
出版National Advisory Committee for Aeronautics, 1957
URLhttp://books.google.com.hk/books?id=1USZAndj35EC&hl=&source=gbs_api
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