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Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach

The interface debonding in carbon fiber-reinforced polymers is analyzed and evaluated using the extended finite element method (XFEM). In order to accurately evaluate the bonding properties between fibers and matrix, different tests were carried out, including the multiple tests for different orient...

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Autores principales: Swati, Raees Fida, Qureshi, Saad Riffat, Sohail, Muhammad Umer, Munir, Adnan, Qureshi, Omer Masood, Khan, Abid Ali
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9413032/
https://www.ncbi.nlm.nih.gov/pubmed/36014148
http://dx.doi.org/10.3390/mi13081226
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author Swati, Raees Fida
Qureshi, Saad Riffat
Sohail, Muhammad Umer
Munir, Adnan
Qureshi, Omer Masood
Khan, Abid Ali
author_facet Swati, Raees Fida
Qureshi, Saad Riffat
Sohail, Muhammad Umer
Munir, Adnan
Qureshi, Omer Masood
Khan, Abid Ali
author_sort Swati, Raees Fida
collection PubMed
description The interface debonding in carbon fiber-reinforced polymers is analyzed and evaluated using the extended finite element method (XFEM). In order to accurately evaluate the bonding properties between fibers and matrix, different tests were carried out, including the multiple tests for different orientations to study longitudinal, transversal, and shear properties of unidirectional carbon fiber-reinforced composites. Extensive experimentation has been performed in all the different groups and categories with different dimensions and parameters in order to ascertain the values of strength and the prediction of the damage to the structure. The experimental and numerical comparison provided significant trends and data to evaluate the mechanical properties of the interface. The values of stiffness and strength are compared and validated. Development of Representative Volume Element (RVE) for progressive damage model to these damage phenomena has already been performed as a feasibility study for the model, though it is not included in this particular paper. The results of this research for all the experimental and numerical sets can serve as reliable data in the microsimulation of devices and sensitive parameters that include carbon fiber-reinforced light metal matrix composites and makes a better investigative model that contributes to various conditions. It further offers an investigation of the microscopic deformation mechanisms in the composites.
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spelling pubmed-94130322022-08-27 Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach Swati, Raees Fida Qureshi, Saad Riffat Sohail, Muhammad Umer Munir, Adnan Qureshi, Omer Masood Khan, Abid Ali Micromachines (Basel) Article The interface debonding in carbon fiber-reinforced polymers is analyzed and evaluated using the extended finite element method (XFEM). In order to accurately evaluate the bonding properties between fibers and matrix, different tests were carried out, including the multiple tests for different orientations to study longitudinal, transversal, and shear properties of unidirectional carbon fiber-reinforced composites. Extensive experimentation has been performed in all the different groups and categories with different dimensions and parameters in order to ascertain the values of strength and the prediction of the damage to the structure. The experimental and numerical comparison provided significant trends and data to evaluate the mechanical properties of the interface. The values of stiffness and strength are compared and validated. Development of Representative Volume Element (RVE) for progressive damage model to these damage phenomena has already been performed as a feasibility study for the model, though it is not included in this particular paper. The results of this research for all the experimental and numerical sets can serve as reliable data in the microsimulation of devices and sensitive parameters that include carbon fiber-reinforced light metal matrix composites and makes a better investigative model that contributes to various conditions. It further offers an investigation of the microscopic deformation mechanisms in the composites. MDPI 2022-07-30 /pmc/articles/PMC9413032/ /pubmed/36014148 http://dx.doi.org/10.3390/mi13081226 Text en © 2022 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Swati, Raees Fida
Qureshi, Saad Riffat
Sohail, Muhammad Umer
Munir, Adnan
Qureshi, Omer Masood
Khan, Abid Ali
Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title_full Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title_fullStr Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title_full_unstemmed Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title_short Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach
title_sort micro-mechanical investigation of interfacial debonding in carbon fiber-reinforced composites using extended finite element method (xfem) approach
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9413032/
https://www.ncbi.nlm.nih.gov/pubmed/36014148
http://dx.doi.org/10.3390/mi13081226
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