| タイトル | Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study I : design and experimental performance of standard turbine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930089493 |
| 著者（英） | Scibbe, Herbert W; Rohlik, Harold E; Wintucky, William T |
| 著者所属（英） | National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. |
| 発行日 | 1957-01-09 |
| 言語 | eng |
| 内容記述 | Detailed design information including overall performance parameters, velocity diagrams, and blade surface velocities is presented. Experimental performance includes maps based on rating as well as total-pressure ratios showing the effect of exit whirl. Also included are results of surveys at the stator exit and downstream of the rotor at design speed and specific work. This information will be used as a standard for comparison with subsequent secondary-flow work. |
| レポートNO | 93R18783
NACA-RM-E56J16 |
| 権利 | No Copyright |
