An efficient complementarity finite element formulation for wrinkling analysis of pneumaric membranes

被引:0
作者
Zhang L. [1 ,2 ]
Cao J.-J. [1 ]
Dong K.-J. [3 ]
Peng F.-J. [4 ]
Yun W.-D. [4 ]
机构
[1] Department of Engineering Mechanics, Chongqing University, Chongqing Key Laboratory of Heterogeneous Material Mechanics, Chongqing
[2] State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an
[3] State Key Laboratory of Structural Analysis for Industrial Equipment, Department of Engineering Mechanics, Dalian University of Technology, Dalian
[4] Shanghai Institute of Aerospace System Engineering, Shanghai
来源
Gongcheng Lixue/Engineering Mechanics | 2020年 / 37卷 / 08期
关键词
Complementarity; Finite deformation; Tension field theory; The co-rotational approach; Wrinkling;
D O I
10.6052/j.issn.1000-4750.2019.09.0533
中图分类号
学科分类号
摘要
Wrinkling deformation is a common instability mode for flexible membrane structures. The numerical simulation on this problem is challenging. Based on the continuum and tension field theory (TFT), a complementarity co-rotational finite element method (FEM) for the wrinkling analysis of pneumatic membrane structures is proposed. By using the co-rotational approach, the finite deformation is decomposed into a rigid body motion in the global coordinate system and small strain deformation in the local coordinate system of the element. The tangent stiffness matrix of a spatial 3-node triangular membrane element is derived. It includes three parts: material stiffness, rotational stiffness and balanced projection stiffness matrices, and covers the influence of a follower load on the elemental stiffness. In the elemental local coordinate system, a wrinkling model is constructed based on the constitutive relation of bi-modulus material, which can judge the status of one element, i.e., 'taut', 'wrinkled' or 'slack'. Furthermore, the oscillation of internal force during the iterative solution is eliminated by establishing an equivalent linear complementarity problem. The stability of the algorithm is improved. Numerical examples show that the proposed method can accurately predict the displacement, stress and wrinkling region of pneumatic membrane structures. Compared with the existing methods such as 'quasi-dynamic' and 'penalty' ways, the proposed method does not require additional solving techniques to ensure convergence. It is convenient for engineering applications. © 2020, Engineering Mechanics Press. All right reserved.
引用
收藏
页码:1 / 9
页数:8
相关论文
共 28 条
[1]  
Xie Chao, Yan Biao, Liu Yu, Et al., High precision manufacturing technology for space-based membrane antennas, Manned Spaceflight, 24, 1, pp. 79-83, (2018)
[2]  
Hu Haiyan, Tian Qiang, Zhang Wei, Et al., Nonlinear dynamics and control of large deployable space structures composed of trusses and meshes, Advances in Mechanics, 43, 4, pp. 390-414, (2013)
[3]  
Li B, Cao Y P, Feng X Q, Et al., Surface wrinkling of mucosa induced by volumetric growth: Theory, simulation and experiment, Journal of the Mechanics and Physics of Solids, 59, pp. 758-774, (2011)
[4]  
Rogers J A, Someya T, Huang Y, Materials and mechanics for stretchable electronics, Science, 327, pp. 1603-1607, (2010)
[5]  
Li B, Cao Y P, Feng X Q, Et al., Mechanics of morphological instabilities and surface wrinkling in soft materials: A review, Soft Matter, 8, 21, pp. 5728-5745, (2012)
[6]  
Li Bo, Studies on surface instability of soft matters, (2011)
[7]  
Wong Y W, Pellegrino S, Wrinkled membranes, Part III: Numerical simulations, Journal of Mechanics of Materials and Structures, 1, 1, pp. 63-95, (2006)
[8]  
Wang C G, Du X W, Tan H F, Et al., A new computational method for wrinkling analysis of gossamer space structures, International Journal of Solids and Structures, 46, 6, pp. 1516-1526, (2009)
[9]  
Wang Changguo, Du Xingwen, He Xiaodong, Bending-wrinkling behavior analysis for inflatable membrane boom, Engineering Mechanics, 26, 2, pp. 210-215, (2009)
[10]  
Wang C G, Tan H F, Experimental and numerical studies on wrinkling control of an inflated beam using SMA wires, Smart Materials and Structures, 19, 10, (2010)