Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle

CORC > 沈阳自动化研究所 > 中国科学院沈阳自动化研究所 > 机器人学研究室

	Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle
	Cui L(崔龙); Wang HW(王洪伟); Jiang T(江涛); Tian, Shen
	2017
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
关键词	flapping wing biplane asymmetric pitching aerodynamics
页码	349-349
通讯作者	Cui L(崔龙)
中文摘要	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.
产权排序	1
会议录	Proceedings of 2017 Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering
语种	英语
内容类型	会议论文
源URL	[http://ir.sia.cn/handle/173321/21341]
专题	沈阳自动化研究所_机器人学研究室
作者单位	Shenyang institute of Automation Chinese Academy of Sciences, Shenyang China
推荐引用方式 GB/T 7714	Cui L,Wang HW,Jiang T,et al. Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle[C]. 见:The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace. Beijing, China. November 20-23, 2017.