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用于超弹性分析的高效杂交应变--EAS固体壳单元的研究
引用本文:郑世杰,佘锦炎.用于超弹性分析的高效杂交应变--EAS固体壳单元的研究[J].计算力学学报,2004,21(3):308-313.
作者姓名:郑世杰  佘锦炎
作者单位:1. 南京航空航天大学,智能材料与结构航空科技重点实验室,江苏,南京,210016
2. 香港大学,机械工程系
基金项目:国家自然科学基金重点项目(50135030);面上项目(10072026)和江苏省自然科学基金(BK2002090)资助项目.
摘    要:提出了一个用于橡胶材料分析的弱变分方程,基于一个可压缩Neo—Hookean模型,将EAS模式和杂交元法有机地结合起来,推导了一个高效、稳定的杂交应变——EAS固体壳单元,通过巧妙地选择应交插值函数和本文中提出的一个精化措施,克服了橡胶材料所表现出的大应变超弹性本构为杂交元正交化法的实施所带来的困难,保证了整个单元列式都仅采用低阶高斯积分,显著提高了计算效率,确保橡胶材料不可压缩性计算的顺利进行,并克服了固体壳元的厚度自锁问题。

关 键 词:超弹性  杂交固体壳  厚度自锁  变分原理  稳定
文章编号:1007-4708(2004)03-0308-06
修稿时间:2002年9月4日

Research of robust hybrid strain-EAS solid shell element for hyperelastic analysis of shells
Zheng Shijie,S.Y. Szee,Nanjing University of Aeronautics & Astronautics,Nanjing,Chin.Research of robust hybrid strain-EAS solid shell element for hyperelastic analysis of shells[J].Chinese Journal of Computational Mechanics,2004,21(3):308-313.
Authors:Zheng Shijie  SY Szee  Nanjing University of Aeronautics & Astronautics  Nanjing  Chin
Institution:Zheng Shijie,S.Y. Szee,Nanjing University of Aeronautics & Astronautics,Nanjing,Chin,.Department of Mechanical Engineering,University of Hongkong
Abstract:The present paper proposes a weaker variational procedure for the large strain analysis of rubber components confining to compressible and incompressible hyperelastic materials of the Neo-Hookean type. The enhanced assumed strain (EAS) modes are incorporated into the hybrid-strain formulation and a robust and stable hybrid strain solid shell element is developed. A refined method is presented and the assumed strain modes are ingeniously selected, so that the orthogonality between the lower order assumed strain modes and higher order ones is realized. The salient feature of the orthogonality for higher computational efficiency is that the higher order assumed strain modes vanish at the sampling points of the second order quadrature and their energy products with the displacement- derived covariant strain can be programmed without resorting to numerical integration. The second major aspect of this contribution is that the whole formulation uses only the second order quadrature, the computational efficiency can be greatly improved and the incompressible locking of hyperelastic materials can be overcome. Furthermore, the present formulation overcomes the thickness locking of the solid shell elements, and its efficacy is illustrated by popular benchmark problems.
Keywords:hyperelastic  hybrid solid shell  thickness locking  variational principle  stabilization
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