| 动力三角翼飞行器气动力设计技术 |
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| 引用本文： | 潘迎春,王洪伟.动力三角翼飞行器气动力设计技术[J].飞行力学,2006,24(3):9-12. |
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| 作者姓名： | 潘迎春 王洪伟 |
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| 作者单位： | 哈尔滨航空工业集团,飞机设计研究所,黑龙江,哈尔滨,150066 |
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| 摘 要： | 介绍了动力三角翼飞行器的总体布局特征及有关气动力设计技术,着重论述了该类飞行器实现飞行稳定性和操纵性的原理,并以某型动力三角翼飞行器的气动力数据为例进行了说明,最后总结出了该类飞行器可行的气动力设计和试验方法。
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| 关 键 词： | 动力三角翼 气动力设计 操纵性 稳定性 平衡速度 |
| 文章编号： | 1002-0853（2006）03-0009-04 |
| 收稿时间： | 2006-02-15 |
| 修稿时间： | 2006-02-152006-05-26 |
Aerodynamic Design Technology for the Trike |
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| PAN Ying-chun,WANG Hong-wei.Aerodynamic Design Technology for the Trike[J].Flight Dynamics,2006,24(3):9-12. |
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| Authors: | PAN Ying-chun WANG Hong-wei |
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| Institution: | Aircraft Design and Research Institute, Harbin Aviation Industry Group, Harbin 150066, China |
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| Abstract: | This paper introduces the general layout characteristics and corresponding aerodynamic design technology for the trike,and put much effort to instruct the trike's stability and control principles with the help of a set of aerodynamic data for a trike.Finally,the applicable aerodynamic design and test methods for the trike are pointed out in this paper. |
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| Keywords: | trike aerodynamic design control stability equilibrium speed |
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