| タイトル | Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860014091 |
| 著者（英） | Putnam, L. E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1986-04-01 |
| 言語 | eng |
| 内容記述 | An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of installing and streamline contouring upper-surface nacelles on the longitudinal aerodynamic characteristics of a high-wing transport configuration. Also investigated were the effects of adding a fairing under the nacelle. The investigation was conducted at free-stream Mach numbers from 0.60 to 0.83 at angles fo attack from -2 deg to 4 deg. Flow-through nacelles were used. Streamline contouring the nacelles substantially reduced the interference drag due to installing the nacelles. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 86N23562
L-16062
NAS 1.60:2579
NASA-TP-2579 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/154351 |
