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X-33 Rev-F Turbulent Aeroheating Results From Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons With Computations
Brian R. Hollis
出版National Aeronautics and Space Administration, Langley Research Center, 2003
URLhttp://books.google.com.hk/books?id=MZI9AQAAMAAJ&hl=&source=gbs_api
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