扑翼MAV翅膀设计及气动力测试研究
文献类型：会议论文
| 作者 | 夏文; 苏刚 |
| 出版日期 | 2012 |
| 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 |
| 关键词 | X型扑翼翅膀 MAV 气动力 翼型设计 |
| 页码 | 3933-3938 |
| 其他题名 | Airfoil design and aerodynamic force testing for flapping-wing Micro Air Vehicles |
| 中文摘要 | 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. |
| 收录类别 | EI |
| 产权排序 | 2 |
| 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 |
| 语种 | 中文 |
| ISBN号 | 978-1-4673-1398-8 |
| 源URL | [http://ir.sia.cn/handle/173321/10492]  |
| 专题 | 沈阳自动化研究所_机器人学研究室 |
| 推荐引用方式 GB/T 7714 | 夏文,苏刚. 扑翼MAV翅膀设计及气动力测试研究[C]. 见:10th World Congress on Intelligent Control and Automation, WCICA 2012. Beijing, China. July 6-8, 2012. |
入库方式： OAI收割
来源：沈阳自动化研究所
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