| 充气结构机翼的设计和试验研究 |
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| 引用本文： | 吕强,叶正寅,李栋.充气结构机翼的设计和试验研究[J].飞行力学,2007,25(4):77-80,85. |
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| 作者姓名： | 吕强 叶正寅 李栋 |
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| 作者单位： | 西北工业大学,航空学院,陕西,西安,710072 |
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| 摘 要： | 为了减少无人机的结构重量,提高雷达隐身能力,充气结构机翼无人机是一种很有发展潜力的飞行器。首先讨论了一种充气机翼的设计方案与加工方法及对应的性能实验,其次着重介绍了充气机翼的翼型生成方法,最后通过实验与试飞论证了充气机翼在飞行中的可行性。
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| 关 键 词： | 充气机翼 充气飞行器 翼型 飞行试验 |
| 文章编号： | 1002-0853（2007）04-0077-04 |
| 收稿时间： | 2006-10-27 |
| 修稿时间： | 2007-05-17 |
Design and Capability Analysis of an Aircraft with Inflatable Wing |
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| LV Qiang,YE Zheng-yin,LI Dong.Design and Capability Analysis of an Aircraft with Inflatable Wing[J].Flight Dynamics,2007,25(4):77-80,85. |
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| Authors: | LV Qiang YE Zheng-yin LI Dong |
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| Abstract: | An inflatable wing aircraft is one type of the promising aircraft for the ability in reducing weight of configuration and avoiding from radar detection.In this paper,we discuss the methods of design,manufacture and experiment testing for one type of the inflatable wing,emphasizing the airfoil generation method.Via experiment and flight tests we prove the feasibility of the inflatable wing in flight. |
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| Keywords: | inflatable wing inflatable aircraft airfoil flight test |
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