| タイトル | The ground effects of a powered-lift STOL aircraft during landing approach |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870014988 |
| 著者（英） | Stevens, Victor C. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1987-02-01 |
| 言語 | eng |
| 内容記述 | The effects of ground proximity on a powered lift STOL aircraft are presented. The data are from NASA's Quiet Short Haul Research Aircraft (QSRA) flown at landing approach airspeeds of less than 60 knots with an 80 lb/sq ft wing loading. These results show that the ground effect change in lift is positive and does significantly reduce the touchdown sink rate. These results are compared to those of the YC-14 and YC-15. The change in drag and pitching moment caused by ground effects is also presented. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 87N24421 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/150044 |
