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Transition of the Laminar Boundary Layer on a Delta Wing with 74 Degree Sweep in Free Flight at Mach Numbers from 2.8 to 5.3
Gary T. Chapman
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=-pHEZ5aN4vAC&hl=&source=gbs_api
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