| タイトル | Design of a 4 1/2 stage turbine with a stage loading factor of 4.66 and high specific work output |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760013058 |
| 著者（英） | Webster, P. F. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | The aerodynamic design of a highly loaded multistage fan drive turbine is discussed. Turbine flowpath and airfoil sections are presented along with respective pressure and velocity distributions. Vibrational modes are identified in the expected turbine operating range. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 76N20146
NASA-CR-2659
PWA-5101 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186590 |
