| タイトル | Preliminary Results of Nene II Engine Altitude-chamber Performance Investigation |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090025338 |
| 著者（英） | Wilsted, H. D.; Vincent, K. R.; Armstron, J. C. |
| 著者所属（英） | National Advisory Committee for Aeronautics |
| 発行日 | 1948-01-01 |
| 言語 | eng |
| 内容記述 | An investigation is being conducted to determine the altitude performance characteristics of the Nene II engine and its components. The present paper presents preliminary results obtained using a jet nozzle of 18.41 inches in diameter, giving an area equal to 96.4 percent of the area of the standard jet nozzle of this engine. The test results presented are for conditions simulating altitudes from seal level to 50,000 feet and ram-pressure ratios from 1.00 to 2.70. The ram pressure ratios correspond to flight Mach numbers between zero and 1.28. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NACA-RM-E8F14 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/260454 |
