Role of the deviation motion on the aerodynamic performance of a mosquito wing in hover

被引:1
|
作者
Jung, Hyunwoo [1 ]
Oh, Sehyeong [1 ]
Choi, Haecheon [1 ,2 ]
机构
[1] Seoul Natl Univ, Dept Mech Engn, Seoul 08826, South Korea
[2] Seoul Natl Univ, Inst Adv Machines & Design, Seoul 08826, South Korea
基金
新加坡国家研究基金会;
关键词
Flapping wing; Insect flight; Deviation motion; Aerodynamics; INSECT FLIGHT; EDGE VORTICES; FORCE; LIFT; GENERATION; ROTATION; DRAG;
D O I
10.1016/j.compfluid.2023.106146
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The deviation angles during wing flapping motions are generally small for many insects and are known to have insignificant or even detrimental effects on the flight performance. Unlike many other insects, a mosquito hovers with a small sweeping amplitude but relatively large deviation angles. Thus, we investigate the effect of a deviation motion ('figure-eight' motion measured by Bomphrey et al. (2017)) on the aerodynamic performance of a mosquito wing in hover by comparing it with that without deviation motion (called in-plane motion). During the stroke, the deviation motion greatly changes the angle of attack and wing moving direction with respect to the stroke plane, but little changes the wing speed. These changes by the deviation motion significantly influence the instantaneous force and power generation. In particular, with the deviation motion, a large drag force is generated at early phase of the downstroke due to the increased angle of attack, and contributes to the vertical force generation. As results, the time-averaged vertical force is increased by the deviation motion, while the time-averaged power required is only slightly increased. Therefore, the mosquito wing generates a larger vertical force more efficiently with the deviation motion, suggesting that a deviation motion may be beneficial for an insect flight with a small sweeping amplitude.
引用
收藏
页数:9
相关论文
共 50 条
  • [1] Effects of wing shape, aspect ratio and deviation angle on aerodynamic performance of flapping wings in hover
    Shahzad, Aamer
    Tian, Fang-Bao
    Young, John
    Lai, Joseph C. S.
    [J]. PHYSICS OF FLUIDS, 2016, 28 (11)
  • [2] Effects of asymmetric stroke deviation on the aerodynamic performance of flapping wing
    Hu, Fujia
    Wang, Yuanying
    Li, Dian
    Liu, Xiaomin
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (02) : 480 - 499
  • [3] Aerodynamic characteristics of flapping motion in hover
    Kurtulus, D. F.
    David, L.
    Farcy, A.
    Alemdaroglu, N.
    [J]. EXPERIMENTS IN FLUIDS, 2008, 44 (01) : 23 - 36
  • [4] Aerodynamic characteristics of flapping motion in hover
    D. F. Kurtulus
    L. David
    A. Farcy
    N. Alemdaroglu
    [J]. Experiments in Fluids, 2008, 44 : 23 - 36
  • [5] Analysis of nonlinear aerodynamic performance and passive deformation of a flexible flapping wing in hover flight
    Chen, Long
    Yang, Feng Liu
    Wang, Yan Qing
    [J]. JOURNAL OF FLUIDS AND STRUCTURES, 2022, 108
  • [6] On the role of vortical structures in aerodynamic performance of a hovering mosquito
    Zhang, Jun-duo
    Huang, Wei-Xi
    [J]. PHYSICS OF FLUIDS, 2019, 31 (05)
  • [7] The Aerodynamic Performance of a Novel Overlapping Octocopter in Hover
    Lei, Yao
    Zhao, Xiangzheng
    [J]. AEROSPACE, 2024, 11 (09)
  • [8] Optimal flapping wing for maximum vertical aerodynamic force in hover: twisted or flat?
    Hoang Vu Phan
    Quang Tri Truong
    Thi Kim Loan Au
    Park, Hoon Cheol
    [J]. BIOINSPIRATION & BIOMIMETICS, 2016, 11 (04)
  • [9] Experimental investigation of the rotor-wing aerodynamic interaction in a tiltwing aircraft in hover
    Droandi, G.
    Zanotti, A.
    Gibertini, G.
    Grassi, D.
    Campariardi, G.
    [J]. AERONAUTICAL JOURNAL, 2015, 119 (1215): : 591 - 612
  • [10] Numerical optimization of helicopter rotor aerodynamic performance in hover
    Le Pape, A
    Beaumier, P
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (03) : 191 - 201