| 推力矢量飞机的起飞性能研究 |
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| 引用本文： | 王衍洋,张守臣,刘志敏,金长江.推力矢量飞机的起飞性能研究[J].飞行力学,2000,18(1):19-21. |
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| 作者姓名： | 王衍洋 张守臣 刘志敏 金长江 |
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| 作者单位： | 北京航空航天大学509教研室,北京,100083 |
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| 摘 要： | 简述推力矢量技术的作用，建立了带三轴推力矢量飞机的起飞滑跑段运动方程，通过数值仿真探讨了推力矢量的偏转大小对起飞性能的影响，对不同推力矢量偏转下飞机起飞性能的仿真计算结果进行了分析。仿真结果表明，采用直接力控制可以明显提高飞机的起飞性能。
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| 关 键 词： | 推力矢量飞机 起飞性能 数值仿真 |
| 修稿时间： | : |
The Influence of Thrust Vectoring on Aircraft Take-Off Performance |
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| Wang Yanyang,Zhang Shouchen,Liu Zhimin,Jin Changjiang.The Influence of Thrust Vectoring on Aircraft Take-Off Performance[J].Flight Dynamics,2000,18(1):19-21. |
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| Authors: | Wang Yanyang Zhang Shouchen Liu Zhimin Jin Changjiang |
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| Abstract: | The important effect of thrust vectoring technology is briefly discussed in this paper. And take off kinematic equations of running take off period of aircraft with three axes of thrust vectoring is given. This paper analyzes the different deflexion angle of thrust vectoring influence on aircraft take off performance according to the result of numerical simulation.The result indicate that direct force can improve take off performance obviously. |
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| Keywords: | thrust vectoring take off performance numerical simulation |
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