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Liu Huixiang, He Guoyi, Wang Qi. NUMERICAL STUDY ON THE AERODYNAMIC PERFORMANCE OF THEFLEXIBLE AND CORRUGATED FOREWING OF DRAGONFLY IN GILDINGFLIGHT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(1): 94-102. doi: 10.6052/0459-1879-18-157
Citation: Liu Huixiang, He Guoyi, Wang Qi. NUMERICAL STUDY ON THE AERODYNAMIC PERFORMANCE OF THEFLEXIBLE AND CORRUGATED FOREWING OF DRAGONFLY IN GILDINGFLIGHT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(1): 94-102. doi: 10.6052/0459-1879-18-157

NUMERICAL STUDY ON THE AERODYNAMIC PERFORMANCE OF THEFLEXIBLE AND CORRUGATED FOREWING OF DRAGONFLY IN GILDINGFLIGHT

doi: 10.6052/0459-1879-18-157
  • Publish Date: 2019-01-18
  • Dragonflies are capable of carrying out dramatic flight manoeuvres, gliding flight is a common mode of flight for dragonfly, and dragonfly wings are the source of dragonflies dramatic flight manoeuvres. Unlike typical engineered airfoil, dragonfly wings are not smooth, wing cross-section are highly corrugated. It has been shown that corrugations could enhance the spanwise stiffness in the wings and influence aerodynamic performance of the dragonfly wings. Flexibility is another characteristic of the dragonfly's wings, which is mainly manifested as the flexible deformation of the wings during the flight. To explore corrugations and flexibility effect on aerodynamic performance of the dragonfly forewings in gliding flight, a computational fluid dynamics (CFD) model and a computational structural mechanics (CSD) model of the corrugated dragonfly forewing are established based on current research, and the modal analysis verified that the model has sufficient accuracy. The corrugated rigid and flexible dragonfly forewing are acquired by using CFD method and CFD/CSD coupling method respectively. The simulation indicated that flexible and corrugated forewings is subjected to aerodynamic load, which only produces bending deformation without torsion deformation in gliding flight, and the aerodynamic response time is short. Compared with the aerodynamic performance of the rigid and corrugated forewings, the result showed that veins and cuticular membrane of flexible forewing are deformed which caused the lift coefficient and drag coefficient decrease, the leading edge vortex of flexible forewing is much higher than rigid forewings at large angle of attack because of deformed vein. The aerodynamic performance of rigid forewings is better below 10 degree angle of attack,and the aerodynamic performance of flexible forewings is better at large angle of attack as result.

     

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  • [1] 刘强, 刘周, 白鹏等. 低雷诺数翼型蒙皮主动振动气动特性及流场结构数值研究. 力学学报, 2016, 48(2): 269-277
    [1] (Liu Qiang, Liu Zhou, Bai Peng, et al.Numerical study about aerodynamic characteristics and flow field structures for a skin of airfoil with active oscillation at low Reynolds number. Chinese Journal of Theoretical and Applied Mechanics, 2016, 48(2): 269-277 (in Chinese))
    [2] 孟令兵, 昂海松, 肖天航. 柔性翼微型飞行器流固耦合数值模拟. 南京航空航天大学学报, 2013, 45(5): 621-627
    [2] (Meng Lingbing, Ang Haisong, Xiao Tianhang.Numerical simulation of fluid-structure interaction for flexible wing MAV. Journal of Nanjing University of Aeronautics & Astronautics, 2013, 45(5): 621-627 (in Chinese))
    [3] Lian Y, Wei S, Viieru D, et al.Membrane wing aerodynamics for micro air vehicles. Progress in Aerospace Sciences, 2003, 39(6): 425-465
    [4] AIAA. Computational modeling of highly flexible membrane wings in micro air vehicles. AIAA Paper2006-1661, 2006
    [5] Jaiman RK, Jiao X, Geubelle PH, et al.Conservative load transfer along curved fluid-solid interface with non-matching meshes. Journal of Computational Physics, 2006, 218(1): 372-397
    [6] Lian Y, Wei S. Three-dimensional fluid-structure interactions of a membrane wing for micro air vehicle applications. AIAA Paper2003-1726, 2003
    [7] Mueller TJ.Fixed and flapping wing dynamics for MAV applications. AIAA Progress in Astron and Aeron, Massachusetts: AIAA Press, 2001: 195
    [8] Liu H, Kawachi K.A numerical study of insect flight. Journal of Computational Physics, 1998, 146(1): 124-156
    [9] Rayner JMV.A new approach to animal flight mechanics. Journal of Experimental Biology, 1979, 80(1): 17-54
    [10] Hu Z, Deng XY.Aerodynamic interaction between forewing and hindwing of a hovering dragonfly. Acta Mechanica Sinica, 2014, 30(6): 787-799
    [11] Kwok M, Mittal R.Experimental investigation of the aerodynamics of a modeled dragonfly wing section. Bulletin of Faculty of Engineering Toyama University, 2005, 5(1): 50-53
    [12] Noda R, Nakata T, Liu H.Effects of wing deformation on aerodynamic performance of a revolving insect wing. Acta Mechanica Sinica, 2014, 30(6): 819-827
    [13] Hamamoto M, Ohta Y, Hara K, et al.Application of fluid--structure interaction analysis to flapping flight of insects with deformable wings. Advanced Robotics, 2007, 21(1-2): 1-21
    [14] Hamamoto M, Ohta Y, Hara K, et al.Free-flight analysis of dragonfly hovering by fluid--structure interaction analysis based on an arbitrary Lagrangian--Eulerian method. Advanced Robotics, 2013, 27(9): 657-666
    [15] 孟令兵, 昂海松, 肖天航. 基于CFD/CSD方法的蜻蜓柔性翼气动特性分析. 航空动力学报, 2014, 29(9): 2063-2069
    [15] (Meng Lingbing, Ang Haisong, Xiao Tianhang.Analysis of aerodynamic characteristics of a flexible wing of dragonfly based on CFD/CSD method. Journal of Aerospace Power, 2014, 29(9): 2063-2069 (in Chinese))
    [16] 郝淑文. 低雷诺数下柔性膜扑翼气动特性的流固耦合分析. [博士论文]. 北京:北京理工大学, 2015
    [16] (Hao Shuwen.Fluid-structure interaction of unsteady aerodynamic of membrane flapping wings at low reynolds number. [PhD Thesis]. Beijing: Beijing Institute of Technology, 2015 (in Chinese))
    [17] Kesel AB.Aerodynamic characteristics of dragonfly wing sections compared with technical aerofoils. Journal of Experimental Biology, 2000, 203: 3125-3135
    [18] Vargas A, Mittal R, Dong H.A computational study of the aerodynamic performance of a dragonfly wing section in gliding flight. Bioinspiration & Biomimetics, 2008, 3(2): 026004
    [19] Rees CJC.Form and function in corrugated insect wings. Nature, 1975, 256(5514): 200-203
    [20] Meng XG, Sun M.Aerodynamic effects of wing corrugation at gliding flight at low Reynolds numbers. Physics of Fluids, 2013, 25(7): 071905
    [21] Zhang Z, Yin Y, Zhong Z, et al.Aerodynamic performance of dragonfly wing with well-designed corrugated section in gliding flight. Computer Modeling in Engineering & Sciences, 2015, 109(3): 285-302
    [22] Dompreh KA, Eghan MJ, Kotsedi L, et al.Comprehensive optical study of the dragonfly Aeshna cyanea, transparent wing. Optics Communications, 2013, 297(12): 176-181
    [23] 赵红晓, 仲政. 蜻蜓翅膀的力学研究进展. 力学季刊, 2009, 30(3): 398-404
    [23] (Zhao Hongxiao, Zhong Zheng.Research advance in mechanical research of dragonfly wings. Chinese Quarterly of Mechanics, 2009, 30(3): 398-404 (in Chinese))
    [24] Okamoto M, Yasuda K, Azuma A.Aerodynamic characteristics of the wings and body of a dragonfly. Journal of Experimental Biology, 1996, 199(2): 281-294
    [25] 孙茂. 昆虫飞行的空气动力学. 力学学报, 2015, 45(2): 1-28
    [25] (Sun Mao.Aerodynamics of inset flight. Chinese Journal of Theoretical and Applied Mechanics, 2015, 45(2): 1-28 (in Chinese))
    [26] Hertel H. Structure, Form, Movement. New York: Reinhold Publishing Corporation, 1966
    [27] Wootton RJ, Newman ADJS.An approach to the mechanics of pleating in dragonfly wings. Journal of Experimental Biology, 1986, 125(1): 361-372
    [28] Newman DJS.The functional wing morphology of some. [PhD Thesis]. Odonata: University of Exeter, 1983
    [29] Antonia BK, Ute P, Werner N.Biomechanical aspects of the insect wing: an analysis using the finite element method. Computers in Biology and Medicine}. 1998, 28: 423-437
    [30] 陈应龙. 蜻蜓翅膀微结构与力学行为的仿生分析研究. [博士论文]. 北京:清华大学, 2012
    [30] (Chen Yinglong.Bionicresearch on the relation between the multi-scaled structure and microstructure and mechanical behavior of dragonfly wing. [PhD Thesis]. Beijing: Tsinghua University, 2012 (in Chinese))
    [31] Dong HB, Christopher K, Liang ZX, et al.An integrated analysis of a dragonfly in free flight//Proceedings of 28th AIAA Applied Aerodynamics Conference, 2010: 4390-4400
    [32] Tong J, Zhao YR, Sun JY, et al.Nanomechanical properties of the stigmaof dragonfly Anax parthenope julius Brauer. Journal of Materials Science, 2007, 42(8):2894-2898
    [33] Ren HH, Wang XS, Li XD, et al.Effects of dragonfly wing structure on the dynamic per formances. Journal of Bionic Engineering, 2013, 10(1): 28-38
    [34] Jongerius SR, Lentink D.Structural analysis of a dragonfly wing. Experimental Mechanics, 2010, 50(9): 1323-1334
    [35] Sudo S, Tsuyuki K, Ikohagi T, et al.A study on the wing structure and flapping behavior of a dragonfly. JSME International Journal Series C Mechanical Systems, Machine Elements and Manufacturing, 1999, 42(3): 721-729
    [36] 李秀娟. 蜻蜓翅膀功能特性力学机制的仿生研究. [博士论文].吉林:吉林大学, 2013
    [36] (Li Xiujuan.Bionic investigation on mechanical mechanism of dragonfly wings functional characteristics. [PhD Thesis]. Jilin: Jilin University, 2013 (in Chinese))
    [37] Shahnazi R, Pariz N, Kamyad AV.Adaptive fuzzy output feedback control for a class of uncertain nonlinear systems with unknown backlash-like hysteresis. Communications in Nonlinear Science & Numerical Simulation, 2010, 15(8): 2206-2221
    [38] 弯艳玲. 蜻蜓翅翼三维空间结构的动力学与疲劳寿命研究. [博士论文]. 吉林:吉林大学, 2010
    [38] (Wan Yanling.Dynamics and fatigue life of three-dimensional structure of dragonfly wings. [PhD Thesis]. Jilin: Jilin University, 2010 (in Chinese))
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