Structural mechanical properties and aerodynamic characteristics of hind wings of cyrtotrachelus buqueti

Shun XU; Pengyu WANG; Shuran CUI; Xiaoming CHEN; Junchong WANG; Chenqi FU

doi:10.13224/j.cnki.jasp.20220091

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Structural mechanical properties and aerodynamic characteristics of hind wings of cyrtotrachelus buqueti

Aerothermodynamics and Aeroengine Design | 更新时间：2025-03-14

- Structural mechanical properties and aerodynamic characteristics of hind wings of cyrtotrachelus buqueti
- Journal of Aerospace Power Vol. 37, Issue 9, Pages: 1824-1834(2022)
- 作者机构：
  
  吉林农业大学工程技术学院，长春 130118
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20220091
  CLC：
- 稿件说明：
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Shun XU, Pengyu WANG, Shuran CUI, et al. Structural mechanical properties and aerodynamic characteristics of hind wings of cyrtotrachelus buqueti[J]. Journal of Aerospace Power, 2022, 37(9): 1824-1834.
DOI：

Shun XU, Pengyu WANG, Shuran CUI, et al. Structural mechanical properties and aerodynamic characteristics of hind wings of cyrtotrachelus buqueti[J]. Journal of Aerospace Power, 2022, 37(9): 1824-1834. DOI： 10.13224/j.cnki.jasp.20220091.

摘要

为研究长足大象甲后翅结构特性和飞行过程的空气动力学特性，建立长足大象甲后翅翅脉特征曲线的数学模型，利用有限元软件对其进行均匀载荷、垂直载荷和扭转载荷3种不同载荷下的静态分析和模态分析。基于嵌套网格法在Fluent软件中模拟后翅上下扑动，分析不同扑动幅值、扭转角度和扑动频率下的后翅升力系数和阻力系数变化规律。结果表明：长足大象甲后翅翅脉分布具有良好的结构刚度和承载能力，在受到不同载荷时，位移和应力的变化较小，结构稳定性较强，并且后翅振动频率为90.312 Hz，与同类昆虫相比，更符合微型扑翼飞行翼研发要求。此外，模拟试验表明长足大象甲后翅可以通过改变扑动幅值、扭转角度和扑动频率来提高升力和推力以实现特技飞行。

Abstract

In order to study the structural characteristics of hind wing and the aerodynamic characteristics during the flight of bamboo weevil

the mathematical model was established based on the characteristic curves of the wing veins of weevil hind wings.By using finite element method

the static structural mechanical properties of hind wing under three different loads （uniform load

vertical load

and torsional load） were researched

and the modal parameters were calculated.The up‑down flapping of the hind wing was simulated in Fluent based on the overlapping mesh method.Aerodynamic characteristics of the hind wing under different flapping amplitude

torsion angle and flapping frequency were analyzed.The results showed that the rib distribution of the hind wing of the bamboo weevil has good structural stiffness and carrying capacity.The displacement and stress changes were small under different loads

and the structural stability was strong.The vibration frequency of the hind wing was 90.312 Hz

which was more in line with the development requirements of the micro flapping wing compared with similar insects.In addition

the simulation results indicated that the hind wing of bamboo weevil can improve the lift and thrust by changing the flutter amplitude

torsion angle and flutter frequency to achieve aerobatic flight.

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Keywords

references

WANG Z J . Dissecting insect flight [J]. Annual Review of Fluid Mechanics , 2005 , 37 : 183 ⁃ 210 .

DUDLEY R . The biomechanics of insect flight:form,function,evolution [J]. Annals of the Entomological Society of America , 2000 , 93 （ 5 ）: 307 ⁃ 308 .

HAAS F , GORB S , WOOTTON R J . Elastic joints in dermapteran hind wings:materials and wing folding [J]. Arthropod Structure and Development , 2000 , 29 （ 2 ）: 137 ⁃ 146 .

YOUNG J , WALKER S M , BOMPHREY R J , et al . Details of insect wing design and deformation enhance aerodynamic function and flight efficiency [J]. Science , 2009 , 325 （ 5947 ）: 1549 ⁃ 1552 .

NGUYEN T T , SUNDAR D S , YEO K S , et al . Modeling and analysis of insect⁃like flexible wings at low Reynolds number [J]. Journal of Fluids and Structures , 2016 , 62 : 294 ⁃ 317 .

马耀鹏 . 基于蠼螋后翅折展机理的空间展开机构设计及其折展性能研究 [D]. 南京：南京航空航天大学 , 2018 .

MA Yaopeng . Design of space deployable mechanism and its folding performance based on the folding mechanism of hind wing of earwigs [D]. Nanjing : Nanjing University of Aeronautics and Astronautics , 2018 . （in Chinese）

WANG C , WANG C , NING Y , et al . Design and mechanical analysis of bionic foldable beetle wings [J]. Applied Bionics and Biomechanics , 2018 ,2018（ 2 ）: 1308465.1 ⁃ 1308465.10 .

WANG C , NING Y , WANG X , et al . Simulation analysis of the aerodynamic performance of a bionic aircraft with foldable beetle wings in gliding flight [J]. Applied Bionics and Biomechanics , 2020 ,2020（ 1 ）: 8843360.1 ⁃ 8843360.12 .

HA N S , TRUONG Q T , GOO N S , et al . Biomechanical properties of insect wings:the stress stiffening effects on the asymmetric bending of the allomyrina dichotoma beetle's hind wing [J]. PLoS One , 2013 , 8 （ 12 ）: 1 ⁃ 10 .

HA N S , NGUYEN Q V , GOO N S , et al . Static and dynamic characteristics of an artificial wing mimicking an allomyrina dichotoma beetle's hind wing for flapping⁃wing micro air vehicles [J]. Experimental Mechanics , 2012 , 52 （ 9 ）: 1535 ⁃ 1549 .

LI Z , SHEN W , TONG G , et al . On the vein⁃stiffening membrane structure of a dragonfly hind wing [J]. Journal of Zhejiang University：Science A , 2009 , 10 （ 1 ）: 72 ⁃ 81 .

史晓君 , 于海业 . 蜻蜓翅膀拱形结构静力学分析 [J]. 安徽农业科学 , 2014 , 42 （ 5 ）: 1395 ⁃ 1397，1400 .

SHI Xiaojun , YU Haiye . Static analysis of dragonfly wing arch structure [J]. Journal of Anhui Agricultural Sciences , 2014 , 42 （ 5 ）: 1395 ⁃ 1397，1400 . （in Chinese）

史晓君 , 于海业 . 蜻蜓翅膀结构刚度有限元分析 [J]. 农业机械学报 , 2012 , 43 （ 1 ）: 224 ⁃ 229,223 .

SHI Xiaojun , YU Haiye . Finite element analysis of dragonfly wing structural stiffness [J]. Transactions of the Chinese Society for Agricultural Machinery , 2012 , 43 （ 1 ）: 224 ⁃ 229,223 . （in Chinese）

REN H , WANG X , LI X , et al . Effects of dragonfly wing structure on the dynamic performances [J]. Journal of Bionic Engineering , 2013 , 10 （ 1 ）: 28 ⁃ 38 .

JONGERIUS S R , LENTINK D . Structural analysis of a dragonfly wing [J]. Experimental Mechanics , 2010 , 50 （ 9 ）: 1323 ⁃ 1334 .

DICKINSON M H , LEHMANN F O , SANE S P . Wing rotation and the aerodynamic basis of insect flight [J]. Science , 1999 , 284 （ 5422 ）: 1954 ⁃ 1960 .

TAY W B . Effect of different types of wing⁃wing interactions in flapping MAVs [J]. Journal of Bionic Engineering , 2017 , 14 （ 1 ）: 60 ⁃ 74 .

LE T Q , VAN TRUONG T , TRAN H T , et al . Two⁃ and three⁃dimensional simulations of beetle hind wing flapping during free forward flight [J]. Journal of Bionic Engineering , 2013 , 10 （ 3 ）: 316 ⁃ 328 .

ENGELS T , KOLOMENSKIY D , SCHNEIDER K , et al . Bumblebee flight in heavy turbulence [J]. Physical Review Letters , 2016 , 116 （ 2 ）: 1 ⁃ 5 .

董强 , 张西金 , 赵宁 , 等 . 蝉翅翼的运动研究与三维数值分析 [J]. 航空动力学报 , 2015 , 30 （ 3 ）: 588 ⁃ 594 .

DONG Qiang , ZHANG Xijin , ZHAO Ning , et al . Motion study and 3D numerical analysis of cicada wing [J]. Journal of Aerodynamics , 2015 , 30 （ 3 ）: 588 ⁃ 594 . （in Chinese）

GREETER J , HEDRICK T L . Direct lateral maneuvers in hawkmoths [J]. Biology Open , 2016 , 5 （ 1 ）: 72 ⁃ 82 .

KUKALOVÁ P J , LAWRENCE J F . Evolution of the hind wing in coleoptera [J]. The Canadian Entomologist , 1993 , 125 （ 2 ）: 181 ⁃ 258 .

许顺 . 长足大象甲的特征、力学、运动特征及其仿生分析 [D]. 长春：吉林大学 , 2017 .

XU Shun . Characteristic,mechanics,movement of crtotrachelus bugueti guer and bionic analysis [D]. Changchun : Jilin University , 2017 . （in Chinese）

LI X , GUO C . Microstructure and material properties of hind wings of a bamboo weevil cyrtotrachelus buqueti （coleoptera:curculionidae） [J]. Microscopy Research and Technique , 2019 , 82 （ 7 ）: 1102 ⁃ 1113 .

HA N S , JIN T L , GOO N S , et al . Anisotropy and non⁃homogeneity of an allomyrina dichotoma beetle hind wing membrane [J]. Bioinspiration and Biomimetics , 2011 , 6 （ 4 ）: 1 ‑ 15 .

JIN T , GOO N S , WOO S C , et al . Use of a digital image correlation technique for measuring the material properties of beetle wing [J]. Journal of Bionic Engineering , 2009 , 6 （ 3 ）: 224 ‑ 231 .

ELLINGTON C P . The aerodynamics of hovering insect flight:Ⅰ the quasi⁃steady analysis [J]. Philosophical Transactions of the Royal Society of London:B Biological Sciences , 1984 , 305 （ 1122 ）: 1 ⁃ 15 .

LI X , GUO C . Wing‑kinematics measurement and flight modelling of the bamboo weevil C.buqueti [J]. IET Nanobiotechnology , 2019 , 14 （ 1 ）: 53 ⁃ 58 .

宁宇 . 仿甲虫微型扑翼飞行器气动特性数值模拟研究 [D]. 郑州：郑州轻工业大学 , 2019 .

NING Yu . Numerical simulation of aerodynamic characteristics of a miniature flapping wing aircraft resembling a beetle [D]. Zhengzhou : Zhengzhou University of Light Industry , 2019 . （in Chinese）

左德参 . 仿生微型飞行器若干关键问题的研究 [D]. 上海：上海交通大学 , 2007 .

ZUO Decan . Research on some key issues of bionic micro air vehicles [D]. Shanghai : Shanghai Jiao Tong University , 2007 . （in Chinese）

ZHAO Y , WANG D , TONG J , et al . Statics analysis of dragonfly wing based on finite element model [J]. Transactions of the Chinese Society of Agricultural Engineering , 2014 , 30 （ 15 ）: 33 ⁃ 38 .

兰世隆 , 孙茂 . 模型昆虫翼作非定常运动时的气动力特性 [J]. 力学学报 , 2001 , 33 （ 2 ）: 173 ⁃ 182 .

LAN Shilong , SUN MAO . Aerodynamic characteristics of model insect wing in unsteady motion [J]. Chinese Journal of Theoretical and Applied Mechanics , 2001 , 33 （ 2 ）: 173 ⁃ 182 . （in Chinese）

杨爱明 , 乔志德 . 用运动嵌套网格方法数值模拟旋翼前飞非定常流场 [J]. 空气动力学学报 , 2000 , 18 （ 4 ）: 427 ⁃ 433 .

YANG Aiming , QIAO Zhide . Numerical simulation of unsteady flow field of rotor forward flight by moving nested mesh method [J]. Acta Aerodynamica Sinica , 2000 , 18 （ 4 ）: 427 ⁃ 433 . （in Chinese）

PROSSER D , BASRAI T , DICKERT J , et al . Wing kinematics and aerodynamics of a hovering flapping micro aerial vehicle [C]∥ Proceedings of Aerospace Conference . Big Sky,US ： IEEE , 2011 : 1 ⁃ 10 .

LI L , HAO Y , XU J , et al . Numerical simulation of unsteady aerodynamic characteristics of the three⁃dimensional composite motion of a flapping wing based on overlapping nested grids [J]. AIP Advances , 2020 , 10 （ 3 ）: 1 ⁃ 13 .

MACHIDA K , SHIMANUKI J . Structure analysis of the wing of a dragonfly [C]∥ Proceedings of 3rd International Conference on Experimental Mechanics and Third Conference of the Asian Committee on Experimental Mechanics . Bellingham，US ： International Society for Optics and Photonics , 2005 : 671 ⁃ 676 .

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