Sandwich Shell Finite Element for Dynamic Explicit Analysis

A. Tabiei, R. Tanov, V. Birman
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Abstract

This work presents the finite element (FE) formulation and implementation of a higher order shear deformable shell element for dynamic explicit analysis of composite and sandwich shells. The formulation is developed using a displacement based third order shear deformation shell theory. Using the differential equilibrium equations and the interlayer requirements, a treatment is developed for the transverse shear, resulting in a continuous, piecewise quartic distribution of the transverse shear stresses through the shell thickness. The FE implementation is cast into a 4-noded quadrilateral shell element with 9 degrees of freedom (DOF) per node. Only C0 continuity of the displacement functions is required in the shell plane, which makes the present formulation applicable to the most common 4-noded bilinear isoparametric shell elements. Expressions are developed for the critical time step of the explicit time integration for orthotropic homogeneous and layered shells based on the developed third order formulation. To assess the performance of the present shell element it is implemented in the general nonlinear explicit dynamic FE code DYNA3D. Several problems are solved and results are compared to other theoretical and numerical results. The developed sandwich shell element is much more computationally efficient for modeling sandwich shells than solid elements.
夹层壳有限元动力显式分析
本工作提出了用于复合材料和夹层壳动力显式分析的高阶剪切变形壳单元的有限元(FE)公式和实现。该公式采用基于位移的三阶剪切变形壳理论。利用微分平衡方程和层间要求,对横向剪切进行了处理,得到横向剪切应力随壳厚的连续分段四次分布。有限元实现是一个4节点的四边形壳单元,每个节点有9个自由度。仅要求位移函数在壳平面上具有C0连续性,这使得本公式适用于最常见的四节点双线性等参壳单元。基于所建立的三阶公式,导出了正交各向异性均匀层状壳显式时间积分的关键时间步长的表达式。为了评估壳单元的性能,采用通用的非线性显式动力有限元程序DYNA3D来实现。解决了几个问题,并与其他理论和数值结果进行了比较。所建立的夹层壳单元比实体单元计算效率高得多。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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