| タイトル | Design and verification of a turbofan swirl augmentor |
| 著者（英） | Shadowen, J. H.; Egan, W. J., Jr. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1978-07-01 |
| 言語 | eng |
| 内容記述 | The paper discusses the details of the design and verification testing of a full-scale turbofan 'swirl' augmentor at sea level and altitude. No flameholders are required in the swirl augmentor since the radial motion of the hot pilot gases and subsequent combustion products provides a continuous ignition front across the stream. Results of rig testing of this full-scale swirl augmentor on an F100 engine, which are very encouraging, and future development plans are presented. The results validate the application of the centrifugal-force swirling flow concept to a turbofan augmentor. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78A43568
AIAA PAPER 78-1040 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/431908 |
