| タイトル | Active control of wing rock of a delta wing at post-stall using tangential leading edge blowing |
| 著者（英） | Roberts, L.; Rock, S. M.; Wood, N. J.; Wong, G. S. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1993-01-01 |
| 言語 | eng |
| 内容記述 | Post-stall roll control utilizing tangential leading edge blowing is demonstrated in a wind tunnel on a delta wing model that exhibited wing rock. The dampening effect of symmetric blowing alone on wing rock is found to be effective up to a certain maximum amount of blowing. A moderate amount of symmetric blowing was shown to be effective in linearizing the asymmetric blowing static rolling moment responses. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 93A20169
AIAA PAPER 93-0056 |
| 権利 | Copyright |
