| タイトル | Quiet Clean Short-haul Experimental Engine (QCSEE) Under-The-Wing (UTW) composite nacelle |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800006860 |
| 著者（英） | Johnston, E. A. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1978-08-01 |
| 言語 | eng |
| 内容記述 | The detail design of the under the wing experimental composite nacelle components is summarized. Analysis of an inlet, fan bypass duct doors, core cowl doors, and variable fan nozzle are given. The required technology to meet propulsion system performance, weight, and operational characteristics is discussed. The materials, design, and fabrication technology for quiet propulsion systems which will yield installed thrust to weight ratios greater than 3.5 to 1 are described. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 80N15119
NASA-CR-135352
R77AEG588 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173715 |
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