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数学与物理学

正交各向异性薄膜沉浮运动流固耦合效应的数值研究

  • 隋晓飞 ,
  • 管子武 ,
  • 鲍麟
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  • 1. 中国科学院大学生物运动力学实验室, 北京 100049;
    2. 中国科学技术大学近代力学系, 合肥 230027

收稿日期: 2013-04-18

  修回日期: 2013-05-20

  网络出版日期: 2014-01-15

基金资助

国家自然科学基金(10602061)资助

Numerical study on the fluid-structure interaction of the heaving orthotropic membrane

  • SUI Xiaofei ,
  • GUAN Ziwu ,
  • BAO Lin
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  • 1 Laboratory for Biomechanics of Animal Locomotion, University of Chinese Academy of Sciences, Beijing 100049, China;
    2 Department of Modern Mechanics, University of Science and Technology of China, Hefei 230027, China

Received date: 2013-04-18

  Revised date: 2013-05-20

  Online published: 2014-01-15

摘要

采用非线性有限单元法和非定常面元法,实现了正交各向异性矩形薄膜在拍动中的流固耦合数值模拟,并研究薄膜在小攻角沉浮运动时,在惯性力和气动力共同作用下的非定常变形响应及对应的气动特性. 结果显示,在相同的沉浮运动条件下,薄膜的柔性有助于改善其气动性能,即薄膜弦向、展向弹性模量减小,引起柔性变形幅度的较大增加,则作用于膜上的平均气动升力也相应显著增高,而平均升力与平均气动功率的比值仅略有降低.

本文引用格式

隋晓飞 , 管子武 , 鲍麟 . 正交各向异性薄膜沉浮运动流固耦合效应的数值研究[J]. 中国科学院大学学报, 2014 , 31(1) : 24 -31 . DOI: 10.7523/j.issn.2095-6134.2014.01.005

Abstract

Fluid-structure interaction of the orthotropic rectangular membrane during heaving motion is simulated numerically by using a nonlinear finite element method combined with an unsteady panel method. The numerical results are analyzed to understand the influence of flexibility on the aerodynamic performance of the heaving membrane at a small angle of attack. It is indicated that the amplitudes of the deformations increase considerably as the chordwise and the spanwise elastic moduli decrease, which leads to an increase of average aerodynamic lifts at the cost of the slight decrease of the ratio of average aerodynamic lift to power.

参考文献

[1] Waszak R M, Jenkins N L, Ifju P. Stability and control properties of an aeroelastic fixed wing micro air vehicle[J]. AIAA, 2001-4005: 2001.

[2] Shyy W, Berg M, Ljungqvist D. Flapping and flexible wings for biological and micro vehicles[J]. Progress in Aerospace Sience, 1999, 35:455-506.

[3] Waszak M R, Davidson J B, Ifju P G. Simulation and flight control of an aeroelastic fixed wing micro air vehicle[J]. AIAA, 2002-4875:2002.

[4] Shyy W, Ifju P, Viieru D. Membrane wing-based micro air vehicles[J].Applied Mechanics Reviews, 2005, 58(4):283-301.

[5] Shyy W, Tang J, Viieru D, et al. Aerodynamics of low Reynolds number flyers[M]. New York: Cambridge University Press, 2008.

[6] Tian X, Iriarte-Diaz J, Middleton K, et al. Direct measurements of the kinematics and dynamics of bat flight[J]. Bioinsp Biomim, 2006, 1: 10-18.

[7] Swartz S M, Grov M S, Kim H D, et al. Mechanical properties of bat wing membrane skin[J]. J Zool Lond, 1996, 239:357-378.

[8] Swartz S M. In bats: phylogeny, morphology, echolocation, and conservation biology[M]. Smithsonian Institution Press, 1998.

[9] Swartz S M, Groves M S, Kim H D, et al. Mechanical properties of bat wing membrane skin[J]. Journal of Zoology, 1996, 239:357-378.

[10] Swartz S M, Diaz J I, Riskin D K, et al. Wing structure and the aerodynamic basis of flight in bats[J]. AIAA, 2007, 1:372-381.

[11] Waldman R M, Song A J, Riskin D K, et al. Aerodynamic behavior of compliant membranes as related to bat flight[J]. AIAA, 2008, 2008-3716:1-13.

[12] Gupta B B. The histology and musculature of plagiopatagium in bats[J]. Mammalia, 1967, 31:313-321.

[13] Zhao L, Huang Q F, Deng X Y, et al. Aerodynamic effects of flexibility in flapping wings[J]. J R Soc Interface, 2010, 7:485-497.

[14] Stanford B, Ifju P, Albertani R, et al. Fixed membrane wings for micro air vehicles: experimental characterization, numerical modeling, and tailoring[J]. Progress in Aerospace Sciences. 2008, 44: 258-294.

[15] Rojratsirikul P, Wang Z, Gursul I. Unsteady aerodynamics of low aspect ratio membrane wings[J]. AIAA, 2010: 729.

[16] Watts P, Mitchell E J, Swartz M S. A computational model for estimating the mechanics of horizontal flapping flight in bats: model description and validation[J]. The Journal of Experimental Biology, 2001, 204: 2873-2898.

[17] Sun Y F, Bao L, Yu Y L. Three-dimensional effects of unsteady flapping rectangular plates[J].Journal of the Gaduate Shool of the Chinese Aademy of Siences, 2010, 27(1):1-9(in Chinese). 孙一峰, 鲍麟, 余永亮.矩形平板典型非定常拍动的三维效应[J]. 中国科学院研究生院学报, 2010, 27(1):1-9.

[18] 王勖成, 邵敏.有限单元法基本原理和数值方法[M].北京:清华大学出版社, 1997.

[19] Van Loon R, Anderson P D, Van de Vosse F N, et al. Comparison of various fluid-structure interaction methods for deformable bodies[J]. Computers & Structures, 2007, 85(11): 833-843.

[20] Wall W A, Genkinger S, Ramm E A. Strong coupling partitioned approach for fluid-structure interaction with free surfaces[J]. Computers & Fluids, 2007, 36(1): 169-183.

[21] Qian R J, Dong S L, Yuan X F. Advances in research on fluid-structure interaction theory[J]. Spatial Structures, 2008, 14(1): 3-15(in Chinese). 钱若军, 董石麟, 袁行飞. 流固耦合理论研究进展[J]. 空间结构, 2008, 14(1): 3-15.

[22] Hubner B, Walhorn E, Dinkler D. Simultaneous solution to the interaction of wind flow and lightweight membrane structures[C]//Warsaw: Proceedings of International Conference on Lightweight Structures in Civil Engineering, 2002: 519-523.

[23] Namkoong K, Choi H G, Yoo J Y. Computation of dynamic fluid-structure interaction in two-dimensional laminar flows using combined formulation[J]. Journal of Fluids and Structures, 2005, 20(1): 51-69.

[24] Matthies H G, Niekamp R, Steindorf J. Algorithms for strong coupling procedures[J]. Computer Methods in Applied Mechanics and Engineering, 2006, 195(17): 2028-2049.

[25] 汪德新. 数学物理方法[M]. 北京:科学出版社, 2006.

[26] Katz J. Caculation of the aerodynamic force on automotive lifting sufaces[J].Journal of Fluids Engineering, 1985, 107(4):438-443.

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