| タイトル | Top-mounted inlet system feasibility for transonic-supersonic fighter aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810015531 |
| 著者（英） | Williams, T. L.; Hunt, B. L.; Nelms, W. P.; Smeltzer, D. B. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1981-04-01 |
| 言語 | eng |
| 内容記述 | The more salient findings are presented of recent top inlet performance evaluations aimed at assessing the feasibility of top-mounted inlet systems for transonic-supersonic fighter aircraft applications. Top inlet flow field and engine-inlet performance test data show the influence of key aircraft configuration variables-inlet longitudinal position, wing leading-edge extension planform area, canopy-dorsal integration, and variable incidence canards-on top inlet performance over the Mach range of 0.6 to 2.0. Top inlet performance data are compared with those or more conventional inlet/airframe integrations in an effort to assess the viability of top-mounted inlet systems relative to conventional inlet installations. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N24066
NASA-TM-81292
A-8575 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/169061 |
