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Experimental Investigation of a Transonic Compressor Rotor with a 1.5-inch Chord Length and an Aspect Ratio of 3.0
其他書名
Design, over-all performance, and rotating-stall characteristics. I
出版National Advisory Committee for Aeronautics, 1955
URLhttp://books.google.com.hk/books?id=FCAkYAAACAAJ&hl=&source=gbs_api