Aerodynamic performance of a bristled wing of a very small insect Dynamically scaled model experiments and computational fluid dynamics simulations using a revolving wing model

被引:29
|
作者
Kolomenskiy, Dmitry [1 ,2 ]
Farisenkov, Sergey [3 ]
Engels, Thomas [4 ]
Lapina, Nadezhda [3 ]
Petrov, Pyotr [3 ]
Lehmann, Fritz-Olaf [4 ]
Onishi, Ryo [1 ]
Liu, Hao [2 ]
Polilov, Alexey [3 ,5 ]
机构
[1] Tokyo Inst Technol, Global Sci Informat & Comp Ctr, Meguro Ku, 2-12-1 O Okayama, Tokyo 1528550, Japan
[2] Chiba Univ, Grad Sch Engn, Inage Ku, 1-33 Yayoicho, Chiba, Chiba 2638522, Japan
[3] Lomonosov Moscow State Univ, Biol Fac, Dept Entomol, Leninskie Gory 1-12, Moscow 119234, Russia
[4] Univ Rostock, Inst Biol Sci, Dept Anim Physiol, Albert Einstein Str 3, D-18059 Rostock, Germany
[5] Joint Russian Vietnamese Trop Res & Technol Ctr, Southern Branch Hem So 3 Duong 3 Thang 2, Ho Chi Minh 70000, Vietnam
基金
俄罗斯基础研究基金会; 俄罗斯科学基金会;
关键词
FLOW; FLIGHT; FORCE; LIFT; CLAP;
D O I
10.1007/s00348-020-03027-0
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Aerodynamic force generation capacity of the wing of a miniature beetleParatuposa placentisis evaluated using a combined experimental and numerical approach. The wing has a peculiar shape reminiscent of a bird feather, often found in the smallest insects. Aerodynamic force coefficients are determined from a dynamically scaled force measurement experiment with rotating bristled and membrane wing models in a glycerin tank. Subsequently, they are used as numerical validation data for computational fluid dynamics simulations using an adaptive Navier-Stokes solver. The latter provides access to important flow properties such as leakiness and permeability. It is found that, in the considered biologically relevant regimes, the bristled wing functions as a less than 50% leaky paddle, and it produces between 66 and 96% of the aerodynamic drag force of an equivalent membrane wing. The discrepancy increases with increasing Reynolds number. It is shown that about half of the aerodynamic normal force exerted on a bristled wing is due to viscous shear stress. The paddling effectiveness factor is proposed as a measure of aerodynamic efficiency. [GRAPHICS] .
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页数:13
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