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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Ullah, Zahur
Durham University
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (23/23 displayed)
- 2024Effects of ply hybridisation on delamination in hybrid laminates at CorTen steel/M79LT-UD600 composite interfaces
- 2024Experimental and numerical investigation of fracture characteristics in hybrid steel/composite and monolithic angle-ply laminates
- 2024Finite fracture mechanics fracture criterion for free edge delamination
- 2023A three-dimensional Finite Fracture Mechanics model for predicting free edge delamination
- 2023A computational framework for crack propagation along contact interfaces and surfaces under loadcitations
- 2023Three-dimensional semi-analytical investigation of interlaminar stresses in composite laminates
- 2023Maritime applications of fibre reinforced polymer composites
- 2023A semi-analytical method for measuring the strain energy release rates of elliptical cracks
- 2023Studies on the impact and compression-after-impact response of ‘Double-Double’ carbon-fibre reinforced composite laminates
- 2023Failure analysis of unidirectional composites under longitudinal compression considering defects
- 2023Exploring the elastic properties of woven fabric composites: a machine learning approach for improved analysis and designcitations
- 2021On the importance of finite element mesh alignment along the fibre direction for modelling damage in fibre-reinforced polymer composite laminatescitations
- 2020Hierarchical finite element-based multi-scale modelling of composite laminatescitations
- 2020Investigation of the free-edge stresses in composite laminates using three-dimensional hierarchic finite elements
- 2020A three-dimensional hierarchic finite element-based computational framework for the analysis of composite laminatescitations
- 2019A unified framework for the multi-scale computational homogenisation of 3D-textile compositescitations
- 2018Mortar Contact Formulation Using Smooth Active Set Strategy Applied to 3D Crack Propagation
- 2018Multiscale Computational Homogenisation of 3D Textile-based Fiber Reinforced Polymer Composites
- 2017Multi-scale Computational Homogenisation to Predict the Long-Term Durability of Composite Structures.citations
- 2016Multi-Scale Computational Homogenisation of the Fibre-Reinforced Polymer Composites Including Matrix Damage and Fibre-Matrix Decohesion
- 2015Hierarchical Finite Element Based Multiscale Computational Homogenisation of Coupled Hygro-Mechanical Analysis for Fibre-Reinforced Polymers
- 2015Multiscale computational homogenisation to predict the long-term durability of composite structures
- 2014Computational homogenisation of fibre reinforced composites
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document
Multi-Scale Computational Homogenisation of the Fibre-Reinforced Polymer Composites Including Matrix Damage and Fibre-Matrix Decohesion
Abstract
A three-dimensional multi-scale computational homogenisation model was developed for the prediction of the nonlinear micro-mechanical response of the fibre-reinforced polymer composite. The two dominant damage mechanisms [1], i.e. matrix damage and fibre-matrix decohesion were considered and modelled using pressure dependent thermodynamically consistent paraboloidal yield criterion and cohesive elements respectively. A linear-elastic transversely isotropic materials model was used to model yarns within the representative volume element (RVE), the principal directions for which were calculated using a potential flow analysis along these yarns. A unified approach [2] was used to impose the RVE boundary conditions, which allows convenient switching between linear displacement, uniform traction and periodic boundary conditions. The developed computational model was implemented within the framework of the hierarchic finite element, which permits the use of arbitrary order of approximation leading to accurate results for relatively coarse meshes. Furthermore, the computational framework was designed to take advantage of distributed memory high-performance computing. The accuracy and efficiency of the developed computational framework were validated with multi-fibre multi-layer M2RVE [3] and single layered plain weave textile composite RVE. In the case of M2RVE, each layer within laminate was represented by a cube with randomly distributed but axially aligned fibres of equal diameters. Elliptical cross sections and cubic splines were used respectively to model the cross sections and paths of the yarns within the textile RVE. The homogenised stress-strain response was validated against the experimental and reference results from the literature. Initiation and propagation of the fibre-matrix interfacial decohesion were also studied. Moreover, the developed computational framework was used to study the effect of fibre-matrix decohesion strength on the homogenised stress-strain response. <br/><br/><br/>Keywords: finite element analysis, fibre reinforced polymer, multiscale computational homogenisation, cohesive zone models, computational plasticity.<br/><br/>References<br/><br/>[1] C. González and J. LLorca. Mechanical behavior of unidirectional fiber-reinforced polymers under transverse compression: microscopic mechanisms and modeling." Composites Science and Technology 67(13): 2795-2806, 2007. <br/><br/>[2] Z. Ullah, Ł. Kaczmarczyk, S. A. Grammatikos, M. C. Evernden and C. J. Pearce. Multi-scale computational homogenisation to predict the long-term durability of composite structures. Computers and Structures, 2015 (Under Review).<br/><br/>[3] G. Soni, R. Singh, M. Mitra and B. G. Falzon. Modelling matrix damage and fibre–matrix interfacial decohesion in composite laminates via a multi-fibre multi-layer representative volume element (M 2 RVE). International Journal of Solids and Structures, 51(2), 449-461, 2014<br/>