Aerodynamic forces and vortical structures of a flapping wing at very low Reynolds numbers

被引:35
|
作者
Lyu, Yu Zhu [1 ]
Zhu, Hao Jie [1 ]
Sun, Mao [1 ]
机构
[1] Beihang Univ, Inst Fluid Mech, Minist Educ, Key Lab Fluid Mech, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
HOVERING INSECT FLIGHT; LIFT; KINEMATICS;
D O I
10.1063/1.5089804
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Reynolds number (Re) for miniature insects is in the range of 80-10. Here, we study how the aerodynamic forces change in this Re range when the flapping mode commonly used by larger insects is employed and explore the physical reasons for the change. We find that at Re below similar to 70, the lift decreases and the drag increases rapidly with decreasing Re. This can be explained as follows. In this Re range, the viscous effect becomes very large. Much of the clockwise (CW) vorticity in the leading-edge vortex is diffused to be far above the wing and moves backward relative to the wing, and some of the counterclockwise (CCW) vorticity in the boundary layer at the lower surface of the wing is diffused to be more forward, and the boundary layer becomes thicker. This results in less CW vorticity moving with the wing and less CCW vorticity moving backward of the wing, causing a reduction in the time rate of change in the vertical component of the total first moment of vorticity, i.e., the reduction in the lift. The above changes in vorticity distributions also increase the vertical distance between the CW vorticity and the CCW vorticity, causing an increase in the time rate of change in the horizontal component of the total first moment of vorticity, i.e., the increase in the drag. These results show that if miniature insects flap their wings as the larger ones do, the aerodynamic forces required for flight cannot be produced and new flapping mode must be used. Published under license by AIP Publishing
引用
收藏
页数:11
相关论文
共 50 条
  • [1] Vortical structures on a flapping wing
    C. A. Ozen
    D. Rockwell
    [J]. Experiments in Fluids, 2011, 50 : 23 - 34
  • [2] Vortical structures on a flapping wing
    Ozen, C. A.
    Rockwell, D.
    [J]. EXPERIMENTS IN FLUIDS, 2011, 50 (01) : 23 - 34
  • [3] Aerodynamic forces and vortical structures in flapping butterfly's forward flight
    Yokoyama, Naoto
    Senda, Kei
    Iima, Makoto
    Hirai, Norio
    [J]. PHYSICS OF FLUIDS, 2013, 25 (02)
  • [4] Aerodynamic Analysis of a Flapping Rotary Wing at a Low Reynolds Number
    Wu, Jianghao
    Wang, Dou
    Zhang, Yanlai
    [J]. AIAA JOURNAL, 2015, 53 (10) : 2951 - 2966
  • [5] Aerodynamic analysis of flapping airfoil propulsion at low reynolds numbers
    Windte, J
    Radespiel, R
    Neef, M
    [J]. Megaflow - Numerical Flow Simulation for Aircraft Design, 2005, 89 : 299 - 313
  • [6] Unsteady aerodynamic forces of a flapping wing
    Wu, JH
    Sun, M
    [J]. JOURNAL OF EXPERIMENTAL BIOLOGY, 2004, 207 (07): : 1137 - 1150
  • [7] Aerodynamic efficiency of a bioinspired flapping wing rotor at low Reynolds number
    Li, H.
    Guo, S.
    [J]. ROYAL SOCIETY OPEN SCIENCE, 2018, 5 (03):
  • [8] On the flowfield and forces generated by a flapping rectangular wing at low Reynolds number
    Ames, R
    Wong, O
    Komerath, N
    [J]. FIXED AND FLAPPING WING AERODYNAMICS FOR MICRO AIR VEHICLE APPLICATIONS, 2002, 195 : 287 - 305
  • [9] Large aerodynamic forces on a sweeping wing at low Reynolds number
    Sun, M
    Wu, JH
    [J]. ACTA MECHANICA SINICA, 2004, 20 (01) : 24 - 31
  • [10] Large aerodynamic forces on a sweeping wing at low Reynolds number
    Sun Mao
    Wu Jianghao
    [J]. Acta Mechanica Sinica, 2004, 20 (1) : 24 - 31