Dean Aamir, Safdar Nabeel, Rolfes Raimund
Institute of Structural Analysis (ISD), Leibniz Universität Hannover, Appelstr. 9A, 30167 Hannover, Germany.
Materials (Basel). 2019 Jun 4;12(11):1816. doi: 10.3390/ma12111816.
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.
几何非线性是对纤维增强聚合物(FRP)进行精确分析时需要考虑的一个方面,因为在其许多结构应用中,如飞机机翼和风力涡轮机叶片中,可能会出现大位移和大旋转。本文提出了一种基于共旋转公式的、基于不变量的各向异性塑性模型的实现方法,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给出。该模型假设了一个与压力相关的各向异性屈服函数,除此之外,还假设了一个非关联塑性势函数,以便对FRP中的实际塑性变形进行建模。然后,将该公式应用于共旋转框架中,以有效地考虑几何非线性效应。通过用户定义材料子程序(UMAT),在商业有限元(FE)软件ABAQUS/Implicit中实现了所开发的模型。简要解释了共旋转框架内的运动学,同时详细讨论了数值处理和实现的重要方面。给出了不同尺度下的代表性数值例子,以证明所提出方法的适用性和鲁棒性。