| タイトル | Rotor redesign for a highly loaded 1800 ft/sec tip speed fan. 1: Aerodynamic and mechanical design report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790017884 |
| 著者（英） | Norton, J. M.; Weber, R. M.; Tari, U. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1979-04-01 |
| 言語 | eng |
| 内容記述 | A quasi three dimensional design system and multiple-circular-arc airfoil sections were used to design a fan rotor. An axisymmetric intrablade flow field calculation modeled the shroud of an isolated splitter and radial distribution. The structural analysis indicates that the design is satisfactory for evaluation of aerodynamic performance of the fan stage in a test facility. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N26055
NASA-CR-159596
PWA-5523-42 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/175221 |
