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A new approach based on undulate propulsion theory for flapping wing analysis and design

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper is aiming for improving new ways of aerodynamic analysis and high efficiency flapping motion design methods of flapping wing aircrafts, or ornithopter. The concept of Undulate Propulsion wave is put forward to better describe propulsive mechanism and it is found to be determinant of flapping wing aerodynamic efficiency. Based on relative conclusion and rigidity theory, a top-down design method for high efficiency flapping wing is extracted. Relationship between passive torsion or active torsion of flapping wing is also analyzed in this paper, and passive torsion is found an easier and more energy-saving way to match the efficiency optimal working point than active torsion. At last, a passive torsion flapping wing ornithopter is introduced, which is designed based on efficiency optimal method presented in this paper. The successful flight test demonstrated that the design method is effective and passive torsion can indeed match the efficiency optimal working point.

源语言英语
主期刊名Proceedings of 2015 International Conference on Fluid Power and Mechatronics, FPM 2015
出版商Institute of Electrical and Electronics Engineers Inc.
781-786
页数6
ISBN(电子版)9781479987702
DOI
出版状态已出版 - 24 11月 2015
活动7th International Conference on Fluid Power and Mechatronics, FPM 2015 - Harbin, 中国
期限: 5 8月 20157 8月 2015

出版系列

姓名Proceedings of 2015 International Conference on Fluid Power and Mechatronics, FPM 2015

会议

会议7th International Conference on Fluid Power and Mechatronics, FPM 2015
国家/地区中国
Harbin
时期5/08/157/08/15

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