Numerical Simulation of the Advantages of the Figure-Eight Flapping Motion of an Insect on Aerodynamics under Low Reynolds Number Conditions

被引:0
作者
Yoshida, Masato [1 ]
Fukui, Tomohiro [2 ]
机构
[1] Kyoto Inst Technol, Dept Masters Program Mechanophys, Matsugasaki Goshokaido Cho,Sakyo Ku, Kyoto 6068585, Japan
[2] Kyoto Inst Technol Matsugasaki, Dept Mech Engn, Goshokaido Cho,Sakyo Ku, Kyoto 6068585, Japan
关键词
unmanned aerial vehicles; hovering motion; elevation angle; Reynolds number; lift coefficient; power coefficient; vortex; LATTICE BOLTZMANN METHOD; EDGE VORTICES; DESIGN; FLIGHT; MECHANISMS; KINEMATICS; FUTURE;
D O I
10.3390/biomimetics9040249
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In proceeding with the advanced development of small unmanned aerial vehicles (UAVs), which are small flying machines, understanding the flight of insects is important because UAVs that use flight are attracting attention. The figure-eight trajectory of the wing tips is often observed in the flight of insects. In this study, we investigated the more efficient figure-eight motion patterns in generating lift during the hovering motion and the relationship between figure-eight motion and Reynolds number. For this purpose, we compared the ratios of the cycle-averaged lift coefficient to the power coefficient generated from each motion by varying the elevation motion angle, which is the rotational motion that represents the figure-eight motion, and the Reynolds number. The result showed that the motion with a smaller initial phase of the elevation motion angle (phi e0 <= 90 degrees) could generate lift more efficiently at all Reynolds numbers. In addition, the figure-eight motion was more effective when the Reynolds number was low.
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页数:23
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