Clap-and-fling mechanism in a hovering insect-like two-winged flapping-wing micro air vehicle

被引:48
|
作者
Hoang Vu Phan [1 ,2 ]
Thi Kim Loan Au [1 ,2 ]
Park, Hoon Cheol [1 ,2 ]
机构
[1] Konkuk Univ, Artificial Muscle Res Ctr, Seoul 143701, South Korea
[2] Konkuk Univ, Dept Adv Technol Fus, Seoul 143701, South Korea
来源
ROYAL SOCIETY OPEN SCIENCE | 2016年 / 3卷 / 12期
基金
新加坡国家研究基金会;
关键词
clap and fling; two-winged flapping-wing micro air vehicle; biomimetics; rhinoceros beetle; insect flight; WEIS-FOGH MECHANISM; TETHERED FLIGHT; TAKE-OFF; AERODYNAMICS; LIFT; KINEMATICS; GENERATION; DEFORMATION; DYNAMICS; DESIGN;
D O I
10.1098/rsos.160746
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
This study used numerical and experimental approaches to investigate the role played by the clap-and-fling mechanism in enhancing force generation in hovering insect-like two-winged flapping-wing micro air vehicle (FW-MAV). The flapping mechanism was designed to symmetrically flap wings at a high flapping amplitude of approximately 192 degrees. The clap-and-fling mechanisms were thereby implemented at both dorsal and ventral stroke reversals. A computational fluid dynamic (CFD) model was constructed based on three-dimensional wing kinematics to estimate the force generation, which was validated by the measured forces using a 6-axis load cell. The computed forces proved that the CFD model provided reasonable estimation with differences less than 8%, when compared with the measured forces. The measurement indicated that the clap and flings at both the stroke reversals augmented the average vertical force by 16.2% when compared with the force without the clap-and-fling effect. In the CFD simulation, the clap and flings enhanced the vertical force by 11.5% and horizontal drag force by 18.4%. The observations indicated that both the fling and the clap contributed to the augmented vertical force by 62.6% and 37.4%, respectively, and to the augmented horizontal drag force by 71.7% and 28.3%, respectively. The flow structures suggested that a strong downwash was expelled from the opening gap between the trailing edges during the fling as well as the clap at each stroke reversal. In addition to the fling phases, the influx of air into the low-pressure region between the wings from the leading edges also significantly contributed to augmentation of the vertical force. The study conducted for high Reynolds numbers also confirmed that the effect of the clap and fling was insignificant when the minimum distance between the two wings exceeded 1.2c (c=wing chord). Thus, the clap and flings were successfully implemented in the FW-MAV, and there was a significant improvement in the vertical force.
引用
收藏
页数:18
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