| タイトル | Experimental study of tail-span effects on a generic canard-controlled missile |
| 著者（英） | Watson, Carolyn B.; Dillon, James L.; Blair, A. B., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1992-01-01 |
| 言語 | eng |
| 内容記述 | An experimental investigation was conducted on a cruciform canard controlled missile configuration to determine the effects of tail span/canard span ratio on controllability. The investigation was conducted over the Mach number range of 1.75 to 3.50. Reductions of tail span/canard span ratio produced lower static margins and higher trim angle of attack. The results show that canard controls can provide pitch- and yaw-control as well as roll-control by proper selection of the tail span/canard span ratio. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 92A22190
AIAA PAPER 92-0079 |
| 権利 | Copyright |
