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Compressive failure of woven fabric reinforced thermoplastic composites with an open-hole: an experimental and numerical study

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H.Liu et al_COST_14-01-2019_Accepted.docxAccepted version3.82 MBMicrosoft WordView/Open
Title: Compressive failure of woven fabric reinforced thermoplastic composites with an open-hole: an experimental and numerical study
Authors: Liu, H
Falzon, B
Li, S
Tan, W
Liu, J
Chai, H
Blackman, B
Dear, J
Item Type: Journal Article
Abstract: This research presents a detailed experimental and numerical study on the compressive failure of woven fabric reinforced thermoplastic composites, with an open-hole and with a pinned open-hole. The experimental evaluations are performed on the composite specimens using the Combined Loading Compression (CLC) evaluation method. Experimental results, including load response and damage morphology, are obtained and analysed. A novel meso-scale damage model is developed, based on Continuum-Damage-Mechanics (CDM), for predicting damage in woven fabric reinforced composites. The developed model, which can capture fibre fracture and matrix cracking, as well as the nonlinear response within the woven composite materials, is employed to conduct virtual Combined Loading Compression (CLC) tests. Numerical simulation results are compared with the extracted experimental results for model validation. Good correlation is achieved between experimental and computational results for both the open-hole and the pinned open-hole, with a two-stage failure process being observed for the pinned open-hole.
Issue Date: 1-Apr-2019
Date of Acceptance: 14-Jan-2019
URI: http://hdl.handle.net/10044/1/67136
DOI: https://dx.doi.org/10.1016/j.compstruct.2019.01.070
ISSN: 1879-1085
Publisher: Elsevier
Start Page: 108
End Page: 117
Journal / Book Title: Composite Structures
Volume: 213
Copyright Statement: © 2019 Elsevier Ltd. All rights reserved. This manuscript is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International Licence http://creativecommons.org/licenses/by-nc-nd/4.0/
Sponsor/Funder: AVIC Manufacturing Technology Institute
Funder's Grant Number: N/A
Keywords: Science & Technology
Technology
Mechanics
Materials Science, Composites
Materials Science
Woven composites
Combined Loading Compression (CLC)
Damage mechanism
Finite Element Analysis (FEA)
VELOCITY IMPACT DAMAGE
INTRALAMINAR FRACTURE-TOUGHNESS
MECHANICS APPROACH
MODELING IMPACT
PART II
BEHAVIOR
DELAMINATION
CURVE
Materials
09 Engineering
Publication Status: Published
Online Publication Date: 2019-01-19
Appears in Collections:Mechanical Engineering
Faculty of Engineering