| 微型扑翼飞行器空气动力学研究进展 |
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| 引用本文： | 李峰,叶正寅,白存儒.微型扑翼飞行器空气动力学研究进展[J].华东交通大学学报,2007,24(1):57-59,84. |
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| 作者姓名： | 李峰 叶正寅 白存儒 |
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| 作者单位： | 西北工业大学,翼型叶栅空气动力学国防科技重点实验室,陕西,西安,710072 |
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| 摘 要： | 微型扑翼飞行器(FMAV)作为一种新概念的航空器,有着广泛的功能和用途,已经受到了各国的高度重视.综述了国内外对微型扑翼飞行器的低雷诺数空气动力学问题的研究现状及未来的发展趋势,讨论了目前研究中需要解决的一些关键技术.在此基础上,总结出今后研究的重点,并为微型扑翼飞行器的设计提供了参考依据.
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| 关 键 词： | 微型扑翼飞行器 气动特性 低雷诺数 非定常流动 |
| 文章编号： | 1005-0523（2007）01-0057-03 |
| 收稿时间： | 2006-06-24 |
| 修稿时间： | 2006-06-24 |
Advances in Aerodynamics Research on Flapping-Wing Micro Air Vehicles |
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| LI Feng,YE Zheng-yin,BAI Cun-ru.Advances in Aerodynamics Research on Flapping-Wing Micro Air Vehicles[J].Journal of East China Jiaotong University,2007,24(1):57-59,84. |
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| Authors: | LI Feng YE Zheng-yin BAI Cun-ru |
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| Abstract: | Flapping-Wing Micro Air Vehicle(FMAV),as a new conceptual vehicle,provides a variety of functions and uses and has attracted much research attention in industrial nations.The present research situation and future development trend of the low Reynolds number aerodynamics of flapping-wing micro air vehicle(FMAV) are surveyed and several key technologies of FMAV are discussed.On this basis,the emphasis of future work of FMAV is summarized and the reference data for future design of FMAV is provided in the end. |
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| Keywords: | flapping-wing micro air vehicle(FMAV) aerodynamic characteristics vlow Reynolds number non-steady flow |
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