タイトル | Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero |
本文(外部サイト) | http://hdl.handle.net/2060/19930089739 |
著者(英) | Maynard, John W , Jr; Westphal, Willard R |
著者所属(英) | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
発行日 | 1957-03-11 |
言語 | eng |
内容記述 | |
レポートNO | 93R19029 NACA-RM-L57A10 |
権利 | No Copyright |
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