Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading

The study quantitatively investigates the mechanical structural behavior and damage mechanisms of composite laminates under low-velocity impacts using Abaqus software. A three-dimensional Puck criterion is utilized to identify the onset of fiber failure and matrix cracking under tensile and compress...

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Published in:Journal of Mechanical Engineering
Main Author: Meon M.S.; Mordi M.F.I.; Mahmud J.
Format: Article
Language:English
Published: UiTM Press 2024
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85215669185&doi=10.24191%2fjmeche.v13i1.2844&partnerID=40&md5=4d304baeca037fce7fba20501eb7ea36
id 2-s2.0-85215669185
spelling 2-s2.0-85215669185
Meon M.S.; Mordi M.F.I.; Mahmud J.
Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
2024
Journal of Mechanical Engineering
13

10.24191/jmeche.v13i1.2844
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85215669185&doi=10.24191%2fjmeche.v13i1.2844&partnerID=40&md5=4d304baeca037fce7fba20501eb7ea36
The study quantitatively investigates the mechanical structural behavior and damage mechanisms of composite laminates under low-velocity impacts using Abaqus software. A three-dimensional Puck criterion is utilized to identify the onset of fiber failure and matrix cracking under tensile and compressive loading conditions. Two progressive damage evolution models are implemented to simulate damage propagation during impact. The model also incorporates cohesive elements with a bilinear traction-separation law to represent interlaminar damage. The performance of the model is validated by comparing its predictions against experimental results for a composite laminate with a stacking sequence of [0°3/45°/-45°2/45°/0°3] subjected to different impact energies (2 J, 4 J, and 8 J). Despite a slight reduction in accuracy at higher energy levels, the model effectively predicts force-displacement curves and energy absorption. The deviation from experimental results is approximately ±6%. This research offers a basis for enhancing the impact resistance and energy absorption characteristics of composite materials. © (2024), (UiTM Press). All rights reserved.
UiTM Press
18235514
English
Article
All Open Access; Bronze Open Access
author Meon M.S.; Mordi M.F.I.; Mahmud J.
spellingShingle Meon M.S.; Mordi M.F.I.; Mahmud J.
Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
author_facet Meon M.S.; Mordi M.F.I.; Mahmud J.
author_sort Meon M.S.; Mordi M.F.I.; Mahmud J.
title Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
title_short Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
title_full Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
title_fullStr Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
title_full_unstemmed Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
title_sort Progressive Damage Model of Carbon-fiber Reinforced Polymer Laminates under Low-velocity Impact Loading
publishDate 2024
container_title Journal of Mechanical Engineering
container_volume 13
container_issue
doi_str_mv 10.24191/jmeche.v13i1.2844
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85215669185&doi=10.24191%2fjmeche.v13i1.2844&partnerID=40&md5=4d304baeca037fce7fba20501eb7ea36
description The study quantitatively investigates the mechanical structural behavior and damage mechanisms of composite laminates under low-velocity impacts using Abaqus software. A three-dimensional Puck criterion is utilized to identify the onset of fiber failure and matrix cracking under tensile and compressive loading conditions. Two progressive damage evolution models are implemented to simulate damage propagation during impact. The model also incorporates cohesive elements with a bilinear traction-separation law to represent interlaminar damage. The performance of the model is validated by comparing its predictions against experimental results for a composite laminate with a stacking sequence of [0°3/45°/-45°2/45°/0°3] subjected to different impact energies (2 J, 4 J, and 8 J). Despite a slight reduction in accuracy at higher energy levels, the model effectively predicts force-displacement curves and energy absorption. The deviation from experimental results is approximately ±6%. This research offers a basis for enhancing the impact resistance and energy absorption characteristics of composite materials. © (2024), (UiTM Press). All rights reserved.
publisher UiTM Press
issn 18235514
language English
format Article
accesstype All Open Access; Bronze Open Access
record_format scopus
collection Scopus
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