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A Co-Rotational Based Anisotropic Elasto–Plastic Model for Geometrically Non-Linear Analysis of Fibre Reinforced Polymer Composites: Formulation and Finite Element Implementation

机译:基于比例关系的各向异性弹塑性模型用于纤维增强聚合物复合材料的几何非线性分析:配方和有限元实现

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摘要

Geometrical non-linearity is one of the aspects to be taken into account for accurate analysis of fibre reinforced polymers (FRPs), since large displacements and rotations may be observed in many of its structural applications such as in aircraft wings and wind turbine blades. In this paper, a co-rotational formulation and implementation of an invariant-based anisotropic plasticity model are presented for geometrically non-linear analysis of FRPs. The anisotropic constitutive equations are formulated in the format of isotropic tensors functions. The model assumes an anisotropic pressure-dependent yield function, and in addition to this, a non-associated plastic potential function in order to model realistic plastic deformations in FRPs. The formulation is then cast in the co-rotational framework to consider the geometrical non-linear effects in an efficient manner. The developed model is implemented in the commercial finite element (FE) software ABAQUS/Implicit via the means of the user-defined material subroutine (UMAT). The kinematics within the co-rotational frame is explained briefly while the important aspects regarding the numerical treatment and implementation are discussed in detail. Representative numerical examples at different scales are presented to demonstrate the applicability and robustness of the proposed development.
机译:几何非线性是精确分析纤维增强聚合物(FRP)时要考虑的方面之一,因为在其许多结构应用(例如飞机机翼和风力涡轮机叶片)中可能会观察到大的位移和旋转。在本文中,提出了基于旋转不变的各向异性塑性模型的同向旋转公式和实现,用于FRP的几何非线性分析。各向异性本构方程以各向同性张量函数的形式表示。该模型假定各向异性压力依赖的屈服函数,此外,还假设一个非关联的塑性势函数,以便对FRP中的实际塑性变形进行建模。然后将该公式投放到同向旋转框架中,以有效地考虑几何非线性效应。通过用户定义的材料子程序(UMAT)在商业有限元(FE)软件ABAQUS / Implicit中实现开发的模型。简要解释了同向旋转框架内的运动学,同时详细讨论了有关数值处理和实现的重要方面。给出了不同规模的代表性数值示例,以证明所提议开发的适用性和鲁棒性。

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