Numerical simulation of a two-dimensional flapping wing in advanced mode

A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for insect's flapping movement, and the model is implemented by the computational fluid dynamics(CFD) software FLUENT and it?s user defined function(UD...

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Published inJournal of hydrodynamics. Series B Vol. 29; no. 6; pp. 1076 - 1080
Main Author 梁志勇;魏亮;卢锦煜;覃小红
Format Journal Article
LanguageEnglish
Published Singapore Elsevier Ltd 01.12.2017
Springer Singapore
College of Science, Donghua University, Shanghai 201620, China%Key Laboratory of Textile Science and Technology, Ministry Education, College of Textiles, Donghua University, Shanghai 201620, China
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Online AccessGet full text
ISSN1001-6058
1878-0342
DOI10.1016/S1001-6058(16)60801-6

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Abstract A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for insect's flapping movement, and the model is implemented by the computational fluid dynamics(CFD) software FLUENT and it?s user defined function(UDF). It is shown that the lift coefficient changes slowly in the intermediate stage, there are two areas in which the lift coefficient changes dramatically, and the drag coefficient behaves quite differently when flapping up and down. The vortex distribution, the pressure distribution, and the velocity vector distribution in the advanced mode at different times follow quite various rules.
AbstractList A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for insect's flapping movement, and the model is implemented by the computational fluid dynamics (CFD) software FLUENT and it's user defined function (UDF). It is shown that the lift coefficient changes slowly in the intermediate stage, there are two areas in which the lift coefficient changes dramatically, and the drag coefficient behaves quite differently when flapping up and down. The vortex distribution, the pressure distribution, and the velocity vector distribution in the advanced mode at different times follow quite various rules.
A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for insect's flapping movement, and the model is implemented by the computational fluid dynamics(CFD) software FLUENT and it?s user defined function(UDF). It is shown that the lift coefficient changes slowly in the intermediate stage, there are two areas in which the lift coefficient changes dramatically, and the drag coefficient behaves quite differently when flapping up and down. The vortex distribution, the pressure distribution, and the velocity vector distribution in the advanced mode at different times follow quite various rules.
Author Wei, Liang
Lu, Jing-yu
Liang, Zhi-yong
Qin, Xiao-hong
AuthorAffiliation College of Science, Donghua University, Shanghai 201620, China;Key Laboratory of Textile Science and Technology, Ministry Education, College of Textiles,Donghua University, Shanghai 201620, China
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CitedBy_id crossref_primary_10_1080_19942060_2019_1652209
crossref_primary_10_1007_s11071_022_07482_8
Cites_doi 10.1017/S0022112090001483
10.4028/www.scientific.net/AMM.555.3
10.1017/jfm.2015.537
10.1016/j.jfluidstructs.2015.03.003
10.1007/BF01090620
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10.1017/S0022112091002197
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10.1242/jeb.201.4.461
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Issue 6
Keywords Numerical simulation
micro flapping wing
dynamic mesh
advanced mode
unsteady aerodynamics
Language English
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Notes 31-1563/T
A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for insect's flapping movement, and the model is implemented by the computational fluid dynamics(CFD) software FLUENT and it?s user defined function(UDF). It is shown that the lift coefficient changes slowly in the intermediate stage, there are two areas in which the lift coefficient changes dramatically, and the drag coefficient behaves quite differently when flapping up and down. The vortex distribution, the pressure distribution, and the velocity vector distribution in the advanced mode at different times follow quite various rules.
Numerical simulation, micro flapping wing, advanced mode, unsteady aerodynamics, dynamic mesh
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PublicationTitle Journal of hydrodynamics. Series B
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College of Science, Donghua University, Shanghai 201620, China%Key Laboratory of Textile Science and Technology, Ministry Education, College of Textiles, Donghua University, Shanghai 201620, China
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Snippet A two-dimensional model is built to describe the translation and the rotation of the hovering flapping movement. The equations of motion are derived for...
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SubjectTerms advanced mode
dynamic mesh
Engineering
Engineering Fluid Dynamics
Hydrology/Water Resources
micro flapping wing
Numerical and Computational Physics
Numerical simulation
Simulation
unsteady aerodynamics
数字模拟;二维;翅膀;液体动力学;用户定义;drag;速度向量;运动
Title Numerical simulation of a two-dimensional flapping wing in advanced mode
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