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题名: 扑翼MAV翅膀设计及气动力测试研究
其他题名: Airfoil design and aerodynamic force testing for flapping-wing Micro Air Vehicles
作者: 夏文 ; 苏刚
作者部门: 机器人学研究室
会议名称: 10th World Congress on Intelligent Control and Automation, WCICA 2012
会议日期: July 6-8, 2012
会议地点: Beijing, China
会议主办者: Academy of Mathematics and Systems Science; IEEE Robotics and Automation Society; IEEE Control Systems Society; National Natural Science Foundation of China; Chinese Association of Automation
会议录: WCICA 2012 - Proceedings of the 18th World Congress on Intelligent Control and Automation
会议录出版者: IEEE
会议录出版地: Piscataway, NJ, United States
出版日期: 2012
页码: 3933-3938
收录类别: EI
ISBN号: 9781467313988
关键词: X型扑翼翅膀 ; MAV ; 气动力 ; 翼型设计
摘要: 我们设计了一款X型扑翼MAV翅膀,并利用自行设计的扑翼MAV气动力测试装置,对不同翅脉布局条件下的扑翼翅膀在不同攻角和不同扑动频率中的气动力情况进行了测试。研究了翅型与气动力的关系,发现X型扑翼MAV翅膀的气动力主要依靠双翅合拢时压缩气体向后喷出而得到:在一定范围内增大X型扑翼MAV翅膀的扑动频率能显著增加翅膀气动力:并且X型扑翼MAV翅膀的气动力随着根梢比和展弦比的减小而增大,成反比关系。
英文摘要: We designed a X-type wing of flapping-wing Micro Air Vehicles (MAV) and doing some aerodynamic force testing by the flapping-wing MAV aerodynamic force testing device which designed by ourselves. In order to study the relationship of aerodynamic force on the flapping-wing models, we do these tests of different flapping-wing models in different angles of attack and flapping frequency. Found that X-wings flapping wing MAV rely mainly on aerodynamic wings folded back when the compressed gas emitted and received; increase the X-wings flapping wing MAV flapping frequency can significantly increase aerodynamic wings; and X-flapping wing MAV Aerodynamic wing root shoot ratio and aspect ratio with the decrease, inversely proportional to the relationship. © 2012 IEEE.
语种: 中文
产权排序: 2
内容类型: 会议论文
URI标识: http://ir.sia.cn/handle/173321/10492
Appears in Collections:机器人学研究室_会议论文

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Recommended Citation:
夏文; 苏刚.扑翼MAV翅膀设计及气动力测试研究.见:IEEE .WCICA 2012 - Proceedings of the 18th World Congress on Intelligent Control and Automation,Piscataway, NJ, United States,2012,3933-3938
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文件名: 扑翼MAV翅膀设计及气动力测试研究.pdf
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