| タイトル | Investigation of powered nacelles on a high aspect ratio NASA supercritical wing, phase 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810010482 |
| 著者（英） | Fournier, P. G.; Patterson, J. C., Jr.; Flechner, S. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1981-02-01 |
| 言語 | eng |
| 内容記述 | A modified wing with the long core separate flow nacelle and several E(3) nacelles was utilized. The effects of nacelle and pylon cant angles and nacelle longitudinal and vertical location were investigated over a Mach number range from 0.70 to 0.83. The results at the cruise condition 0.82 Mach number and 0.55 lift coefficient are presented. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 81N19008 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/568217 |
