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Article

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

1
Department of Master’s Program of Mechanophysics, Kyoto Institute of Technology Matsugasaki Goshokaido-cho, Sakyo-ku, Kyoto 606-8585, Japan
2
Department of Mechanical Engineering, Kyoto Institute of Technology Matsugasaki Goshokaido-cho, Sakyo-ku, Kyoto 606-8585, Japan
*
Author to whom correspondence should be addressed.
Biomimetics 2024, 9(4), 249; https://doi.org/10.3390/biomimetics9040249
Submission received: 25 February 2024 / Revised: 17 April 2024 / Accepted: 18 April 2024 / Published: 20 April 2024
(This article belongs to the Special Issue Bio-Inspired Design and Control of Unmanned Aerial Vehicles (UAVs))

Abstract

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 (φe090°) could generate lift more efficiently at all Reynolds numbers. In addition, the figure-eight motion was more effective when the Reynolds number was low.
Keywords: unmanned aerial vehicles; hovering motion; elevation angle; Reynolds number; lift coefficient; power coefficient; vortex unmanned aerial vehicles; hovering motion; elevation angle; Reynolds number; lift coefficient; power coefficient; vortex

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MDPI and ACS Style

Yoshida, M.; Fukui, T. Numerical Simulation of the Advantages of the Figure-Eight Flapping Motion of an Insect on Aerodynamics under Low Reynolds Number Conditions. Biomimetics 2024, 9, 249. https://doi.org/10.3390/biomimetics9040249

AMA Style

Yoshida M, Fukui T. Numerical Simulation of the Advantages of the Figure-Eight Flapping Motion of an Insect on Aerodynamics under Low Reynolds Number Conditions. Biomimetics. 2024; 9(4):249. https://doi.org/10.3390/biomimetics9040249

Chicago/Turabian Style

Yoshida, Masato, and Tomohiro Fukui. 2024. "Numerical Simulation of the Advantages of the Figure-Eight Flapping Motion of an Insect on Aerodynamics under Low Reynolds Number Conditions" Biomimetics 9, no. 4: 249. https://doi.org/10.3390/biomimetics9040249

APA Style

Yoshida, M., & Fukui, T. (2024). Numerical Simulation of the Advantages of the Figure-Eight Flapping Motion of an Insect on Aerodynamics under Low Reynolds Number Conditions. Biomimetics, 9(4), 249. https://doi.org/10.3390/biomimetics9040249

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