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Performance of a Supersonic Mixed-flow Rotor with a Swept Leading Edge and 0.52 Inlet Radius Ratio

Arthur W. GoldsteinRalph L. Schacht

出版	National Advisory Committee for Aeronautics, 1953
URL	http://books.google.com.hk/books?id=rCcoSwAACAAJ&hl=&source=gbs_api