| タイトル | Development of non-conventional control methods for high angle of attack flight using vortex manipulation |
| 著者（英） | Malcolm, Gerald N.; Ng, T. Terry; Murri, Daniel G.; Lewis, Liane C. |
| 著者所属（英） | Eidetics International, Inc.|NASA Langley Research Center |
| 発行日 | 1989-01-01 |
| 言語 | eng |
| 内容記述 | Low-speed wind tunnel experiments have been conducted to define methods for the manipulation of a generic fighter forebody's vortices in order to generate controlled yawing moments at high alpha. Attention is given to two vortex-control schemes: one involving independently controlled forebody tip strakes, and the other individually controlled blowing ports on the forebody. The most effective methods for forebody yawing-moment control were found to be the minimization of natural asymmetry with a pair of symmetrically mounted tip strakes, and the perturbation of the vortex system away from the symmetric condition with asymmetric blowing. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 89A47653
AIAA PAPER 89-2192 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/362118 |
