| タイトル | Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790024993 |
| 著者（英） | Leavitt, L. D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1979-10-01 |
| 言語 | eng |
| 内容記述 | The Langley V/STOL tunnel was used to determine the effects of vectoring exhaust flow on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration. Vectoring was accomplished by blowing from over-wing-mounted engines over a variable trailing-edge flap. Effects of varying canard geometry and wing leading-edge geometry were investigated. Wind-tunnel data were obtained at a Mach number of 0.186 for an angle-of-attack range from -20 deg to 24 deg and engine nozzle pressure ratios from 1.0 (jet off) to approximately 3.75. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79N33164
L-13108
NASA-TP-1533 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174503 |
