| 三翼面飞机与直接力控制 |
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| 引用本文： | 邱菊.三翼面飞机与直接力控制[J].飞机设计,2005(4):7-10. |
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| 作者姓名： | 邱菊 |
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| 作者单位： | 成都飞机工业(集团)公司,成都,610092 |
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| 摘 要： | 简要介绍了三翼面布局的飞机以及直接力控制的基本原理,某三翼面战斗机气动计算证实了直接力控制的可行性,最后总结了三翼面布局。
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| 关 键 词： | 三翼面布局 三翼面飞机 直接力控制 |
| 修稿时间： | 2005年7月30日 |
Three-surface Aircraft and Direct Lift Control |
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| Qiu Ju.Three-surface Aircraft and Direct Lift Control[J].Aircraft Design,2005(4):7-10. |
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| Authors: | Qiu Ju |
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| Abstract: | This paper briefly presents three-surface(canard wing horizontal tail) aircraft and the basic principle of direct lift control.The feasibility of direct lift control has been verified in the paper by aerodynamic calculation of a three-surface fighter.Finally,the three-surface configuration is discussed. |
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| Keywords: | three-surface configuration three-surface aircraft direct lift control |
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