| 飞机大攻角俯仰飞行的稳定域分析 |
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| 引用本文： | 邹毅,姚宏.飞机大攻角俯仰飞行的稳定域分析[J].空军工程大学学报,2006,7(4):11-12. |
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| 作者姓名： | 邹毅 姚宏 |
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| 作者单位： | 国防科技大学，空军工程大学理学院 湖南长沙410073，空军工程大学理学院，陕西西安710051，陕西西安710051 |
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| 摘 要： | 基于大攻角飞行条件下的动力学方程,定性分析了飞机在大攻角条件下作俯仰飞行的动力学特性。提出了在不同参数匹配条件下的飞行稳定性,并据此划分了飞机的飞行稳定域。
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| 关 键 词： | 大攻角 俯仰飞行 稳定域 |
| 文章编号： | 1009-3516（2006）04-0011-02 |
| 收稿时间： | 2005-04-18 |
| 修稿时间： | 2005-04-18 |
Stable Field Analysis of Aircraft Flying at High Angles of Attack |
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| ZOU Yi,YAO Hong.Stable Field Analysis of Aircraft Flying at High Angles of Attack[J].Journal of Air Force Engineering University(Natural Science Edition),2006,7(4):11-12. |
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| Authors: | ZOU Yi YAO Hong |
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| Institution: | 1.National University of Defense Technolgy,changsha,Hunan 410073,China;2.The Science Institute, Air Force Engineering University, Xi''an, Shaanxi 710051, China |
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| Abstract: | Based on dynamics equation of aircraft flying at high angles of attack,the dynamical characteristics of aircraft flying at pitching on condition of high angles of attack are qualitatively analyzed.The flying stabilities are raised on the basis of various matching parameters,and then the stable field of aircraft can be divided. |
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| Keywords: | high angle of attack pitching flying stable field |
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