| タイトル | Design and performance of a 427-meter-per-second-tip-speed two-stage fan having a 2.40 pressure ratio |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780025166 |
| 著者（英） | Cunnan, W. S.; Stevans, W.; Urasek, D. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1978-10-01 |
| 言語 | eng |
| 内容記述 | The aerodynamic design and the overall and blade-element performances are presented of a 427-meter-per-second-tip-speed two-stage fan designed with axially spaced blade rows to reduce noise transmitted upstream of the fan. At design speed the highest recorded adiabatic efficiency was 0.796 at a pressure of 2.30. Peak efficiency was not established at design speed because of a damper failure which terminated testing prematurely. The overall efficiencies, at 60 and 80 percent of design speed, peaked at approximately 0.83. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N33109
NASA-TP-1314
E-9005 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/177587 |
