| 连翼布局飞机及探测无人机研究进展 |
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| 引用本文： | 郑诚行.连翼布局飞机及探测无人机研究进展[J].飞行力学,2006,24(4):1-5. |
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| 作者姓名： | 郑诚行 |
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| 作者单位： | 成都飞机设计研究所1室,四川,成都,610041 |
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| 摘 要： | 在收集、整理、分析国外连翼布局飞机研究资料的基础上,介绍了国外连翼布局飞机的研究历程和设计特点;特别是基于近年来对未来战场信息情报、监视、侦察任务的需求,介绍了连翼布局探测无人机这一新的作战概念和装备技术的研究进展情况。
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| 关 键 词： | 连翼布局 探测无人机 多学科优化 气动弹性 |
| 文章编号： | 1002-0853(2006)04-0001-05 |
| 收稿时间： | 2005-09-22 |
| 修稿时间： | 2006-08-14 |
Research and Development on Joined Wing Aircraft and Sensorcraft |
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| ZHENG Cheng-xing.Research and Development on Joined Wing Aircraft and Sensorcraft[J].Flight Dynamics,2006,24(4):1-5. |
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| Authors: | ZHENG Cheng-xing |
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| Institution: | The First Department, Chengdu Aircraft Design and Research Institute, Chengdu 610041, China |
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| Abstract: | On the basis of collecting,trimming,and analyzing the overseas research information about joined wing aircraft,this paper presents the research history and design characteristics of joined wing aircraft.Especially recent years,according to the requirements of intelligence,surveillance,reconnaissance(ISR) tasks of future war field,it is also present the research and development for the new campaign concept and equipment technique of joined wing sensorcraft. |
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| Keywords: | joined wing sensorcraft MDO aeroelasticity |
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