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几种基于组合方法的复合材料层合板壳单元
引用本文:尹进,杨东生,张盛,陈飙松,董锴.几种基于组合方法的复合材料层合板壳单元[J].航空学报,2013,34(1):86-96.
作者姓名:尹进  杨东生  张盛  陈飙松  董锴
作者单位:1. 大连理工大学运载工程与力学学部工程力学系,辽宁大连,116024
2. 大连理工大学运载工程与力学学部工程力学系,辽宁大连 116024;大连理工大学工业装备结构分析国家重点实验室,辽宁大连 116024
3. 北京宇航系统工程研究所,北京,100076
基金项目:国家自然科学基金(11072050,51021140004);国家基础性发展规划项目(2010CB832704);国家“863”计划(2012AA050901);中央高校基本科研业务费专项资金~~
摘    要: 为了方便合适地选取单元进行工程分析,本文基于开放式结构有限元分析系统SiPESC.FEMS,提出一种基于经典模型的复合材料层合板壳单元程序计算框架。此框架利用组合的方法,考虑平面壳单元中板、膜单元之间的关系以及程序编制过程中的重用性、灵活性等特点,采用了软件设计中的构造器(Builder)模式实现不同的复合材料层合板壳单元。本框架具有一定的通用性和可扩展性,能够处理复杂荷载、边界条件及三维空间不同材料铺设方向的层合板壳的结构分析问题。基于此方法实现了5种复合材料层合板壳单元,通过数值算例分析对比讨论各单元性能,显示了本框架具有简单实用等特点以及采用组合方法构造单元的优势。

关 键 词:复合材料  层合板壳单元  组合式单元  有限元  SiPESC  
收稿时间:2012-02-20;

Laminated Composite Plate and Shell Elements Based on Combination Method
YIN Jin , YANG Dongsheng , ZHANG Sheng , CHEN Biaosong , DONG Kai.Laminated Composite Plate and Shell Elements Based on Combination Method[J].Acta Aeronautica et Astronautica Sinica,2013,34(1):86-96.
Authors:YIN Jin  YANG Dongsheng  ZHANG Sheng  CHEN Biaosong  DONG Kai
Institution:1.Department of Engineering Mechanics,Faculty of Vehicle Engineering and Mechanics, Dalian University of Technology,Dalian 116024,China 2.State Key Laboratory of Structural Analysis for Industrial Equipment,Dalian University of Technology,Dalian 116024,China 3.Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China
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.
Keywords:composite  laminated plate and shell elements  combined element  finite element  SiPESC
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