几种基于组合方法的复合材料层合板壳单元

doi:10.7527/S1000-6893.2013.0011

Abstract

Abstract:

Based on the open style finite element system SiPESC.FEMS, a computational software framework of laminated composite plate and shell elements is constructed in this paper according to the classic model in order to select composite elements properly in engineering analysis. With the employment of the combinational method of plate and membrane elements, a software design pattern called builder is proposed for laminated multiple composite plate and shell elements. This software design framework possesses good versatility and extensibility. Furthermore, it can handle complex boundary conditions of load and displacement, and be applied to 3D laminated composite structures with different ply angles and materials as well. Five kinds of laminated composite plate and shell elements are implemented in this simple and practical unified software framework. Numerical examples of these elements are presented to validate their precision and the advantage of the combination method.

Key words: composite, laminated plate and shell elements, combined element, finite element, SiPESC

CLC Number:

YIN Jin, YANG Dongsheng, ZHANG Sheng, CHEN Biaosong, DONG Kai. Laminated Composite Plate and Shell Elements Based on Combination Method[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(1): 86-96.

References

[1] Fan Y Q, Zhang L H. New development of extra large composite aircraft components application technology—advance of aircraft manufacture technology. Acta Aeronautica et Astronautica Sinica, 2009, 30(3): 534-543. (in Chinese) 范玉青, 张丽华. 超大型复合材料机体部件应用技术的新进展——飞机制造技术的新跨越. 航空学报, 2009, 30(3): 534-543.

[2] Liu G X, Wang Z M. Review about finite elements of multilayer plates and shells. Advances in Mechanics, 1984, 14(4): 415-419. (in Chinese) 刘国玺, 王震鸣. 复合材料多层板壳有限元研究现状. 力学进展, 1984, 14(4): 415-419.

[3] Hong Z Q. A review of finite element techniques in laminated plates and shells. Acta Materiae Compositae Sinica, 1985, 2(2): 80-89. (in Chinese) 洪志泉. 复合材料迭层板壳有限单元法现状分析. 复合材料学报, 1985, 2(2): 80-89.

[4] Zhang Y X, Yang C H. Recent developments in finite element analysis for laminated composite plates. Composite Structures, 2009, 88(1): 147-157.

[5] Carrera E, Miglioretti F, Petrolo M. Accuracy of refined finite elements for laminated plate analysis. Composite Structures, 2011, 93(5): 1311-1327.

[6] Yang H T Y, Saigal S, Masud A, et al. A survey of recent shell finite elements. International Journal for Numerical Methods in Engineering, 2000, 47(1-3): 101-127.

[7] Zhang H W, Chen B S, Li Y P, et al. Advancement of design and implementation of SiPESC for development of integrated CAE software systems. Computer Aided Engineering, 2011, 20(2): 39-49. (in Chinese) 张洪武, 陈飙松, 李云鹏, 等. 面向集成化CAE软件开发的SiPESC研发工作进展. 计算机辅助工程, 2011, 20(2): 39-49.

[8] Shen G L, Hu G K. Mechanics of composite materials. Beijing: Tsinghua University Press, 2006: 88-93. (in Chinese) 沈观林, 胡更开. 复合材料力学. 北京: 清华大学出版社, 2006: 88-93.

[9] Xu Y, Long Y Q. Conforming triangular membrane element with vertex rotational freedom from generalized compatible condition. Engineering Mechanics, 1993, 10(2): 31-39. (in Chinese) 须寅, 龙驭球. 采用广义协调条件构造具有旋转自由度的三角形膜元. 工程力学, 1993, 10(2): 31-39.

[10] Batoz J L, Bathe K J, Ho L W. A study of three node triangular plate bending elements. International Journal for Numerical Methods in Engineering, 1980, 15(12): 1771-1812.

[11] Wang X C. Finite element method. Beijing: Tsinghua University Press, 2003: 343-347. (in Chinese) 王勖成. 有限单元法. 北京: 清华大学出版社, 2003: 343-347.

[12] Chen W J, Cheung Y K. Refined triangular discrete Kirchhoff plate element for thin plate bending, vibration and buckling analysis. International Journal for Numerical Methods in Engineering, 1998, 41(8): 1507-1525.

[13] Soh A K, Ling C. An improved discrete Kirchhoff triangular element for bending, vibration and buckling analyses. European Journal of Mechanics A: Solids, 2000, 19(5): 891-910.

[14] Zhang S, Yang D S, Yin J, et al. Design pattern of element computation module of SiPESC.FEMS. Computer Aided Engineering, 2011, 20(3): 46-52. (in Chinese) 张盛, 杨东生, 尹进, 等. SiPESC.FEMS的单元计算模块设计模式. 计算机辅助工程, 2011, 20(3): 46-52.

[15] Zhang C Z. Analytical theory of plate and shell composite mechanics. Beijing: National Defense Industry Press, 2009: 223-229. (in Chinese) 张承宗. 复合材料板壳力学解析理论. 北京: 国防工业出版社, 2009: 223-229.

Laminated Composite Plate and Shell Elements Based on Combination Method

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