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

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Original languageEnglish
Article number1816
JournalMATERIALS
Volume12
Issue number11
Publication statusPublished - 1 Jun 2019

Abstract

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.

Keywords

    Anisotropic plasticity, Co-rotational framework, Finite element method (FEM), FRPs composites

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title = "A Co-Rotational Based Anisotropic Elasto–Plastic Model for Geometrically Non-Linear Analysis of Fibre Reinforced Polymer Composites: Formulation and Finite Element Implementation ",
abstract = "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.",
keywords = "Anisotropic plasticity, Co-rotational framework, Finite element method (FEM), FRPs composites",
author = "Aamir Dean and Nabeel Safdar and Raimund Rolfes",
note = "Funding information: Acknowledgments: This paper is dedicated to the memory of late Matthias Vogler, a great talent that has sadly left us too soon. The authors gratefully acknowledge the helpful comments and discussions with Jose Reinoso, Eelco Jansen, Sven Scheffler and Benedikt Daum. AD is grateful to Yaqin Ali for the language revision of the manuscript. The publication of this article was funded by the Open Access Fund of the Leibniz Universit{\"a}t Hannover.",
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doi = "10.3390/ma12111816",
language = "English",
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journal = "MATERIALS",
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T2 - Formulation and Finite Element Implementation

AU - Dean, Aamir

AU - Safdar, Nabeel

AU - Rolfes, Raimund

N1 - Funding information: Acknowledgments: This paper is dedicated to the memory of late Matthias Vogler, a great talent that has sadly left us too soon. The authors gratefully acknowledge the helpful comments and discussions with Jose Reinoso, Eelco Jansen, Sven Scheffler and Benedikt Daum. AD is grateful to Yaqin Ali for the language revision of the manuscript. The publication of this article was funded by the Open Access Fund of the Leibniz Universität Hannover.

PY - 2019/6/1

Y1 - 2019/6/1

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AB - 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.

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