| タイトル | Effect of simulated in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810021548 |
| 著者（英） | Capone, F. J.; Bare, E. A.; Berrier, B. L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1981-08-01 |
| 言語 | eng |
| 内容記述 | Investigations were conducted in the Langley 16-Foot Transonic Tunnel to provide data on a 0.10-scale model of the prototype F-18 airplane and a 0.047-scale model of the F-15 three-surface configuration (canard, wing, and horizontal tails). Test data were obtained at static conditions and at Mach numbers from 0.6 to 1.2 over an angle-of-attack range from 2 deg to 15 deg. Nozzle pressure ratio was varied from jet off to about 8.0. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 81N30086
NASA-TP-1890
L-14531 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/168276 |
