复合材料夹层壳有限元新公式

A. Tabiei, R. Tanov
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引用次数: 1

摘要

提出了夹层壳有限元计算公式。夹心壳元件配方允许正交异性面和芯材。夹层壳单元基于一阶壳体剪切变形理论,该理论是大多数各向同性材料壳体有限元所采用的。因此,所提出的程序可用于任何可用的壳单元在商业有限元软件包。该公式基于夹层壳单元和典型均质壳单元之间的应力和弯矩结果等式。在非线性有限元程序DYNA3D中实现了所开发的单元,对其精度、效率和综合性能进行了验证和检验。预测结果与更为复杂和计算量大得多的三维分析结果一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
New Formulation for Composite Sandwich Shell Finite Element
Sandwich shell finite element formulation is developed and presented. The sandwich shell element formulation allows for orthotropic faces and core material. The sandwich shell element is based on first shell order shear deformable theory utilized by most shell finite elements for isotropic materials. Consequently, the presented procedure can be adopted for any shell element available in commercial finite element packages. The formulation is based on the equalities of stress and moment resultants between a sandwich shell element and a typical homogenous shell element. The developed element is implemented in the nonlinear finite element code DYNA3D to validate and check its accuracy, efficiency and overall performance. The predicted results show good agreement with results obtained from far more complicated and computationally intensive 3-D analyses.
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