Numerical comparison between symmetric and asymmetric flapping wing in tandem configuration

被引:4
作者
Liu, Fangyuan [1 ]
Li, Song [1 ,2 ]
Xiang, Jinwu [1 ,3 ]
Li, Daochun [1 ]
Tu, Zhan [4 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China
[2] City Univ Hong Kong, Dept Biomed Engn, Kowloon, Hong Kong, Peoples R China
[3] Tianmushan Lab Xixi Octagon City, Hangzhou, Peoples R China
[4] Beihang Univ, Inst Unmanned Syst, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
FOREWING-HINDWING INTERACTION; FLIGHT; AERODYNAMICS; ROTATION;
D O I
10.1063/5.0200547
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Dragonflies show impressive flight performance due to their unique tandem flapping wing configuration. While previous studies focused on forewing-hindwing interference in dragonfly-like flapping wings, few have explored the role of asymmetric pitching angle in tandem flapping wings. This paper compares the aerodynamic performance of asymmetric dragonfly-like wings with symmetric hummingbird-like wings, both arranged in tandem. Using a three-dimensional numerical model, we analyzed wing configurations with single/tandem wings, advance ratios (J) from 0 to 0.45, and forewing-hindwing phase differences ( phi) from 0 degrees to 180 degrees at a Reynolds number of 7000. Results show that asymmetric flapping wings exhibit higher vertical force and flight efficiency in both single and tandem wing configurations. Increasing the phase difference ( phi) improves flight efficiency with minimal loss of vertical force in the asymmetric flapping mode, while the symmetrical flapping mode significantly reduces vertical force at a 180 degrees phase difference. Additionally, symmetric tandem flapping wings unexpectedly gain extra vertical force during in-phase flapping. This study uncovers the flow characteristics of dragonfly-like tandem flapping wings, providing a theoretical basis for the design of tandem flapping wing robots.
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页数:20
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