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Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle
Jiang T(江涛); Wang HW(王洪伟); Tian, Shen; Cui L(崔龙)
作者部门机器人学研究室
会议名称The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace
会议日期November 20-23, 2017
会议地点Beijing, China
会议录名称Proceedings of 2017 Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering
2017
页码349-349
产权排序1
关键词Flapping Wing Biplane Asymmetric Pitching Aerodynamics
摘要The aerodynamics of flapping wing micro air vehicle (FMAV) are significantly affected by the wing kinematics, of which are mainly flapping and pitching of the wings. And the design of wing kinematics pattern is an effective way to modulate the lift and thrust, consequently the control the vehicle. Here, such pattern of wing motion for hovering flapping flight is studied using computational fluid dynamics (CFD). This work is highlighted by the insights into asymmetric pitching and the effects of it on the aerodynamic performance. It is found that the thrust benefits from this wing kinematics configuration and the lift is also greatly influenced by this. Explanation of these phenomenon are discussed. And other important factors relating to the design of a practical FMAV are also noted.
语种英语
文献类型会议论文
条目标识符http://ir.sia.cn/handle/173321/21341
专题机器人学研究室
通讯作者Cui L(崔龙)
作者单位Shenyang institute of Automation Chinese Academy of Sciences, Shenyang China
推荐引用方式
GB/T 7714
Jiang T,Wang HW,Tian, Shen,et al. Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle[C],2017:349-349.
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