| タイトル | Vortex Lift Augmentation by Suction |
| 著者（英） | Jackson, L. R.; Taylor, A. H.; Huffman, J. K. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-08-01 |
| 言語 | eng |
| 内容記述 | Lift performance is improved on a 60 degrees swept Gothic wing. Vortex lift at moderate to high angles of attack on highly swept wings used to improve takeoff performance and maneuverability. New design proposed in which suction of propulsion system augments vortex. Turbofan placed at down stream end of leading-edge vortex system induces vortex to flow into inlet which delays onset of vortex breakdown. |
| NASA分類 | MECHANICS |
| レポートNO | 83B10071
LAR-12969 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/408412 |
