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Flow Field Resulting from Forward-facing Nozzles Exhausting Near a Large Cylindrical Body at Free-stream Mach Numbers of 3.0, 4.5, and 6.0
James A. MartinRobert J. McGhee
出版National Aeronautics and Space Administration, 1971
URLhttp://books.google.com.hk/books?id=VdcUIgsm7IoC&hl=&source=gbs_api
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