| タイトル | Investigation of a 0.6 Hub-tip Radius-ratio Transonic Turbine Designed for Secondary-flow Study IV : Rotor Loss Patterns as Determined by Hot-wire Anemometers with Rotor Operating in a Circumferentially Uniform Inlet Flow Field |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930090032 |
| 著者（英） | Allen, Hubert W; Kofskey, Milton G |
| 著者所属（英） | National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. |
| 発行日 | 1958-05-20 |
| 言語 | eng |
| 内容記述 | |
| レポートNO | 93R19322
NACA-RM-E58B27 |
| 権利 | No Copyright |
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