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Effects of Three Outlet-annulus Area Blockage Configurations on the Performance of a 20-inch (50.8-CM) Axial-flow Compressor Rotor
Walter Martin OsbornGeorge W. Lewis (Jr.)
出版National Aeronautics and Space Administration, 1969
URLhttp://books.google.com.hk/books?id=kc0f2KVLdRsC&hl=&source=gbs_api
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