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
相关论文
共 50 条
  • [1] Clap-and-Fling Mechanism in Non-Zero Inflow of a Tailless Two-Winged Flapping-Wing Micro Air Vehicle
    Au, Loan Thi Kim
    Park, Hoon Cheol
    Lee, Seok Tae
    Hong, Sung Kyung
    [J]. AEROSPACE, 2022, 9 (02)
  • [2] Effects of wing kinematics, corrugation, and clap-and-fling on aerodynamic efficiency of a hovering insect-inspired flapping-wing micro air vehicle
    Nguyen, Khanh
    Au, Loan Thi Kim
    Phan, Hoang-Vu
    Park, Soo Hyung
    Park, Hoon Cheol
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 118
  • [3] Controlled hovering flight of an insect-like tailless flapping-wing micro air vehicle
    Hoang Vu Phan
    Kang, Taesam
    Park, Hoon Cheol
    [J]. 2017 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS (ICM), 2017, : 74 - 78
  • [4] Development of an Insect-like Flapping-Wing Micro Air Vehicle with Parallel Control Mechanism
    Chen, Zihao
    Zhang, Weiping
    Mou, Jiawang
    Zhao, Jiaxin
    [J]. APPLIED SCIENCES-BASEL, 2022, 12 (07):
  • [5] Experimental investigation of wing flexibility on force generation of a hovering flapping wing micro air vehicle with double wing clap-and-fling effects
    Nguyen, Quoc V.
    Chan, Woei L.
    Debiasi, Marco
    [J]. INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2017, 9 (03) : 187 - 197
  • [6] Experimental Study on the Wing Parameter Optimization of Flapping-Wing Aircraft Based on the Clap-and-Fling Mechanism
    Li, Qian
    Ji, Aihong
    Shen, Huan
    Li, Renshu
    Liu, Kun
    Zheng, Xiangming
    Shen, Lida
    Han, Qingfei
    [J]. INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2022, 23 (02) : 265 - 276
  • [7] Bioinspired low-noise wing design for a two-winged flapping-wing micro air vehicle
    [J]. 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (56):
  • [8] Bioinspired Low-Noise Wing Design for a Two-Winged Flapping-Wing Micro Air Vehicle
    Lu, Zhenbo
    Debiasi, Marco
    Quoc-Viet Nguyen
    Chan, Woei-Leong
    [J]. AIAA JOURNAL, 2018, 56 (12) : 4697 - 4705
  • [9] Experimental Study on the Wing Parameter Optimization of Flapping-Wing Aircraft Based on the Clap-and-Fling Mechanism
    Qian Li
    Aihong Ji
    Huan Shen
    Renshu Li
    Kun Liu
    Xiangming Zheng
    Lida Shen
    Qingfei Han
    [J]. International Journal of Aeronautical and Space Sciences, 2022, 23 : 265 - 276
  • [10] Remotely Controlled flight of an Insect-like Tailless Flapping-wing Micro Air Vehicle
    Phan, Hoang Vu
    Park, Hoon Cheol
    [J]. 2015 12TH INTERNATIONAL CONFERENCE ON UBIQUITOUS ROBOTS AND AMBIENT INTELLIGENCE (URAI), 2015, : 315 - 317