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Robust layerwise C-0 finite element approach based on a variable separation method for the modeling of composite and sandwich plates

机译:基于可变分离方法的鲁棒分层C-0有限元方法用于复合材料和夹心板的建模

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This paper deals with a new approach using both the variable separation and a robust C-0 eight-node finite element for the modeling of composite plates. The displacement field is approximated as a sum of separated functions of the in-plane coordinates x, y and the transverse coordinate z. This choice yields to an iterative process that consists of solving a 2D and 1D problem successively at each iteration. In the thickness direction, a fourth-order expansion in each layer is considered. For the in-plane description, the main novelty consists in the formulation of a field compatible approximation for the transverse shear strain field, referred to as the CL8 interpolation. This latter has to be adapted to the particular framework of the separated representation. It allows us to eliminate the shear locking pathology by constraining only the z-constant transverse shear strain terms. Numerical assessments show the absence of locking problems as well as the enhanced robustness with respect to distorted element shapes in comparison to classical isoparametric approaches. This new CL8 plate element provides excellent convergence rates under different boundary and loading conditions, and it yields accurate displacements and stresses for both thick and thin composite and sandwich plates.
机译:本文研究了一种使用变量分离和鲁棒的C-0八节点有限元对复合板进行建模的新方法。位移场近似为平面内坐标x,y和横向坐标z的分离函数之和。这种选择产生了一个迭代过程,该过程包括在每次迭代时依次解决2D和1D问题。在厚度方向上,考虑了每层中的四阶膨胀。对于平面内描述,主要新颖之处在于制定了横向剪切应变场的场兼容近似法,称为CL8插值法。后者必须适合于分离表示的特定框架。它允许我们仅通过约束z常数横向剪切应变项来消除剪切锁定病理。数值评估表明,与经典的等参方法相比,不存在锁定问题,并且在扭曲的元件形状方面具有更高的鲁棒性。这种新型的CL8板元件在不同的边界和载荷条件下均具有出色的收敛速度,并且可为厚,薄复合板和夹心板产生精确的位移和应力。

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