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 in | Journal of hydrodynamics. Series B Vol. 29; no. 6; pp. 1076 - 1080 |
|---|---|
| Main Author | |
| Format | Journal Article |
| Language | English |
| 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 |
| Subjects | |
| Online Access | Get full text |
| ISSN | 1001-6058 1878-0342 |
| DOI | 10.1016/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. |
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| 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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| Author_xml | – sequence: 1 fullname: 梁志勇;魏亮;卢锦煜;覃小红 |
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| 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 10.1016/j.jfluidstructs.2013.02.001 10.1017/S0022112091002197 10.1063/1.858173 10.1016/j.compfluid.2015.04.009 10.1242/jeb.201.4.461 |
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| Copyright | 2017 Publishing House for Journal of Hydrodynamics China Ship Scientific Research Center 2017 Copyright © Wanfang Data Co. Ltd. All Rights Reserved. |
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| Keywords | Numerical simulation micro flapping wing dynamic mesh advanced mode unsteady aerodynamics |
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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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| References | Lin, Lin, Sun (bib18) 2016; 28 Zhang, Chang, Duan (bib2) 2009; 27 Wang, Sun, Zhang (bib19) 2015; 74 Zaitsev, Sharina (bib1) 1983; 18 Yang, Wang, Xue (bib10) 2015; 99 Nakata, Liu, Bomphrey (bib7) 2015; 783 Liu, Ellington, Kawachi (bib13) 1998; 201 Tay, Van Oudheusden, Bijl (bib9) 2015; 55 Banazadeh, Taymourtash (bib11) 2014; 555 Bai, Cuie, Li (bib3) 2007; 25 Zhang, Shang, Zhang (bib17) 2016; 35 Ohmi, Coutanceau, Loc (bib4) 1990; 211 Lan, Sun (bib14) 2001; 33 Ohmi, Coutanceau, Daube (bib5) 1991; 225 Triantafyllou, Triantafyllou, Gopalkrishnan (bib6) 1991; 3 Zhao, Liu, Zhu (bib12) 2005; 35 Zhou, Lin (bib16) 2006; 38 Tay, DENG, Van Oudheusden (bib8) 2015; 115 Lu, Xie, Zhang (bib15) 2013; 39 Zhang, Wang, Sheng (bib20) 2015; 74 Wang, Sun, Zhang (CR19) 2015; 74 Nakata, Liu, Bomphrey (CR7) 2015; 783 Zhang, Wang, Sheng (CR20) 2015; 74 Ohmi, Coutanceau, Loc (CR4) 1990; 211 Bai, Cuie, Li (CR3) 2007; 25 Ohmi, Coutanceau, Daube (CR5) 1991; 225 Banazadeh, Taymourtash (CR11) 2014; 555 Liu, Ellington, Kawachi (CR13) 1998; 201 Zhou, Lin (CR16) 2006; 38 Lu, Xie, Zhang (CR15) 2013; 39 Zaitsev, Sharina (CR1) 1983; 18 Zhang, Chang, Duan (CR2) 2009; 27 Zhang, Shang, Zhang (CR17) 2016; 35 Tay, Deng, Van Oudheusden (CR8) 2015; 115 Tay, Van Oudheusden, Bijl (CR9) 2015; 55 Lin, Lin, Sun (CR18) 2016; 28 Zhao, Liu, Zhu (CR12) 2005; 35 Lan, Sun (CR14) 2001; 33 Triantafyllou, Triantafyllou, Gopalkrishnan (CR6) 1991; 3 Yang, Wang, Xue (CR10) 2015; 99 S L Lan (29061076_CR14) 2001; 33 L P Zhang (29061076_CR2) 2009; 27 K Ohmi (29061076_CR4) 1990; 211 A Banazadeh (29061076_CR11) 2014; 555 A A Zaitsev (29061076_CR1) 1983; 18 T Nakata (29061076_CR7) 2015; 783 W B Tay (29061076_CR9) 2015; 55 W Yang (29061076_CR10) 2015; 99 W B Tay (29061076_CR8) 2015; 115 S Q Wang (29061076_CR19) 2015; 74 K Ohmi (29061076_CR5) 1991; 225 L Zhang (29061076_CR20) 2015; 74 J Lin (29061076_CR18) 2016; 28 C H Zhou (29061076_CR16) 2006; 38 P Bai (29061076_CR3) 2007; 25 M S Triantafyllou (29061076_CR6) 1991; 3 P F Zhao (29061076_CR12) 2005; 35 H Liu (29061076_CR13) 1998; 201 K Lu (29061076_CR15) 2013; 39 L Zhang (29061076_CR17) 2016; 35 |
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10.1063/1.858173 – volume: 38 start-page: 1403 issue: 9 year: 2006 end-page: 1405 ident: CR16 article-title: Numerical study on aerodynamic performance of flapping wings [J] publication-title: Journal of Harbin Institute of Technology – volume: 115 start-page: 226 year: 2015 end-page: 242 ident: CR8 article-title: Validation of immersed boundary method for the numerical simulation of flapping wing flight [J] publication-title: Computers and Fluids doi: 10.1016/j.compfluid.2015.04.009 – volume: 74 start-page: 1058 issue: C year: 2015 end-page: 1064 ident: CR19 article-title: The effects of roll motion of the floating platform on hydrodynamics performance of horizontal-axis tidal current turbine [J] publication-title: Journal of Marine Science and Technology – volume: 28 start-page: 1 issue: 6 year: 2016 end-page: 11 ident: CR18 article-title: Modelling hydrodynamic processes in tidal stream energy extraction [J] publication-title: Journal of Hydrodynamics – volume: 99 start-page: 1506 issue: 1 year: 2015 ident: 29061076_CR10 publication-title: Procedia Engineering – volume: 28 start-page: 1 issue: 6 year: 2016 ident: 29061076_CR18 publication-title: Journal of Hydrodynamics – volume: 38 start-page: 1403 issue: 9 year: 2006 ident: 29061076_CR16 publication-title: Journal of Harbin Institute of Technology – volume: 783 start-page: 323 year: 2015 ident: 29061076_CR7 publication-title: Journal of Fluid Mechanics doi: 10.1017/jfm.2015.537 – volume: 74 start-page: 796 issue: C year: 2015 ident: 29061076_CR20 publication-title: Journal of Marine Science and Technology – volume: 35 start-page: 1 issue: 2 year: 2016 ident: 29061076_CR17 publication-title: Journal of Hydroelectric Engineering – volume: 115 start-page: 226 year: 2015 ident: 29061076_CR8 publication-title: Computers and Fluids doi: 10.1016/j.compfluid.2015.04.009 – volume: 25 start-page: 175 issue: 2 year: 2007 ident: 29061076_CR3 publication-title: Acta Aerodynamica Sinica – volume: 201 start-page: 461 issue: 4 year: 1998 ident: 29061076_CR13 publication-title: Journal of Experimental Biology doi: 10.1242/jeb.201.4.461 – volume: 211 start-page: 37 year: 1990 ident: 29061076_CR4 publication-title: Journal of Fluid Mechanics doi: 10.1017/S0022112090001483 – volume: 555 start-page: 3 year: 2014 ident: 29061076_CR11 publication-title: Applied Mechanics and Materials doi: 10.4028/www.scientific.net/AMM.555.3 – volume: 225 start-page: 607 year: 1991 ident: 29061076_CR5 publication-title: Journal of Fluid Mechanics doi: 10.1017/S0022112091002197 – volume: 33 start-page: 173 issue: 2 year: 2001 ident: 29061076_CR14 publication-title: Acta Mechanica Sinica – volume: 39 start-page: 76 issue: 5 year: 2013 ident: 29061076_CR15 publication-title: Journal of Fluids and Structures doi: 10.1016/j.jfluidstructs.2013.02.001 – volume: 18 start-page: 554 issue: 4 year: 1983 ident: 29061076_CR1 publication-title: Fluid Dynamics doi: 10.1007/BF01090620 – volume: 35 start-page: 441 issue: 4 year: 2005 ident: 29061076_CR12 publication-title: Journal of University of Science and Technology of China – volume: 74 start-page: 1058 issue: C year: 2015 ident: 29061076_CR19 publication-title: Journal of Marine Science and Technology – volume: 55 start-page: 237 year: 2015 ident: 29061076_CR9 publication-title: Journal of Fluids and Structures doi: 10.1016/j.jfluidstructs.2015.03.003 – volume: 27 start-page: 246 issue: 2 year: 2009 ident: 29061076_CR2 publication-title: Acta Aerodynamica Sinica – volume: 3 start-page: 2835 issue: 12 year: 1991 ident: 29061076_CR6 publication-title: Physics of Fluids A-Fluid Dynamics doi: 10.1063/1.858173 |
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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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