Loading…
Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate
•Micro-residual stresses reduce effective ply strength in constrained conditions.•Ply residual stresses can achieve more than 50 % of failure load.•Thick ply laminates tend to retrieve more ply residual stresses.•Thin ply laminate exhibits higher strength and lower crack opening after failure. Durin...
Saved in:
Published in: | Composite structures 2023-09, Vol.319, p.117158, Article 117158 |
---|---|
Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3 |
---|---|
cites | cdi_FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3 |
container_end_page | |
container_issue | |
container_start_page | 117158 |
container_title | Composite structures |
container_volume | 319 |
creator | Goncalves, Paulo Teixeira Arteiro, Albertino Rocha, Nuno |
description | •Micro-residual stresses reduce effective ply strength in constrained conditions.•Ply residual stresses can achieve more than 50 % of failure load.•Thick ply laminates tend to retrieve more ply residual stresses.•Thin ply laminate exhibits higher strength and lower crack opening after failure.
During the manufacturing of thermoset-based carbon fiber reinforced polymers (CFRPs), micro-residual stresses are developed in the material, due a mismatch of the chemical-thermal-mechanical properties of the fibers and the polymer matrix. This ultimately leads to a reduction in the mechanical performance of the composite material. In this work, a representative volume element (RVE) of a composite sub-laminate with a 90° ply discretized at micro-scale level, stacked within homogenized plies, is proposed to study the micro-residual stresses and the ply mechanical response considering the in-situ effect caused by the constraining adjacent layers. A model framework is developed using finite elements in Abaqus®/Standard with user-subroutines. The retrieved micro-residual stresses in the 90° layer are generated by the dissimilar chemical shrinkage and thermal expansions, plus the additional residual meso-scale stresses caused by the constraining effect of adjacent plies. The residual stresses in the constrained condition can achieve almost 80 % of the ply failure load for the 0/90/0 sub-laminate, meaning lower sub-laminate strain to failure. Thick laminates retrieve more residual stresses in the transverse 90° layer and exhibit lower constrained strength and more unstable post-failure response, demonstrating that thin-ply laminates exhibit beneficial constraining effects during the curing process. |
doi_str_mv | 10.1016/j.compstruct.2023.117158 |
format | article |
fullrecord | <record><control><sourceid>elsevier_cross</sourceid><recordid>TN_cdi_crossref_primary_10_1016_j_compstruct_2023_117158</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0263822323005020</els_id><sourcerecordid>S0263822323005020</sourcerecordid><originalsourceid>FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3</originalsourceid><addsrcrecordid>eNqFkM1OwzAQhH0AiVJ4B79AUtv5M0eo-JOKuMDZsjdr6pI4lZ0icuLVcSgSR06r3dHMjj5CKGc5Z7xe7XIY-n0cwwHGXDBR5Jw3vJInZMFEXWRSiOKMnMe4Y4zJkvMF-XpyEIasR9hq70B3VHvdTdFFOlg6bpGitQjjvO27KV0cvHuMSfYUDsH5N9r_RASMrj2kgPQ_6Rip81RT0MEMfoX74XOic70huhFpp3vn9YgX5NTqLuLl71yS17vbl_VDtnm-f1xfbzIoajlmxpbCWFkZZplupS2xMFrWVtQVNGiEqNEKTGfbcFMJEGV51UiQNRQMWmOKJZHH3FQ1xoBW7YPrdZgUZ2qGp3bqD56a4akjvGS9OVox9ftwGFQEhx6wdSGRUe3g_g_5Blm0hHQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate</title><source>ScienceDirect Journals</source><creator>Goncalves, Paulo Teixeira ; Arteiro, Albertino ; Rocha, Nuno</creator><creatorcontrib>Goncalves, Paulo Teixeira ; Arteiro, Albertino ; Rocha, Nuno</creatorcontrib><description>•Micro-residual stresses reduce effective ply strength in constrained conditions.•Ply residual stresses can achieve more than 50 % of failure load.•Thick ply laminates tend to retrieve more ply residual stresses.•Thin ply laminate exhibits higher strength and lower crack opening after failure.
During the manufacturing of thermoset-based carbon fiber reinforced polymers (CFRPs), micro-residual stresses are developed in the material, due a mismatch of the chemical-thermal-mechanical properties of the fibers and the polymer matrix. This ultimately leads to a reduction in the mechanical performance of the composite material. In this work, a representative volume element (RVE) of a composite sub-laminate with a 90° ply discretized at micro-scale level, stacked within homogenized plies, is proposed to study the micro-residual stresses and the ply mechanical response considering the in-situ effect caused by the constraining adjacent layers. A model framework is developed using finite elements in Abaqus®/Standard with user-subroutines. The retrieved micro-residual stresses in the 90° layer are generated by the dissimilar chemical shrinkage and thermal expansions, plus the additional residual meso-scale stresses caused by the constraining effect of adjacent plies. The residual stresses in the constrained condition can achieve almost 80 % of the ply failure load for the 0/90/0 sub-laminate, meaning lower sub-laminate strain to failure. Thick laminates retrieve more residual stresses in the transverse 90° layer and exhibit lower constrained strength and more unstable post-failure response, demonstrating that thin-ply laminates exhibit beneficial constraining effects during the curing process.</description><identifier>ISSN: 0263-8223</identifier><identifier>DOI: 10.1016/j.compstruct.2023.117158</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Finite element analysis (FEA) ; Micro-mechanics ; Polymer matrix composites (PMCs) ; Residual/internal stress ; Thermomechanical</subject><ispartof>Composite structures, 2023-09, Vol.319, p.117158, Article 117158</ispartof><rights>2023 The Author(s)</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3</citedby><cites>FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3</cites><orcidid>0000-0003-2427-0243 ; 0000-0002-7779-2558</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Goncalves, Paulo Teixeira</creatorcontrib><creatorcontrib>Arteiro, Albertino</creatorcontrib><creatorcontrib>Rocha, Nuno</creatorcontrib><title>Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate</title><title>Composite structures</title><description>•Micro-residual stresses reduce effective ply strength in constrained conditions.•Ply residual stresses can achieve more than 50 % of failure load.•Thick ply laminates tend to retrieve more ply residual stresses.•Thin ply laminate exhibits higher strength and lower crack opening after failure.
During the manufacturing of thermoset-based carbon fiber reinforced polymers (CFRPs), micro-residual stresses are developed in the material, due a mismatch of the chemical-thermal-mechanical properties of the fibers and the polymer matrix. This ultimately leads to a reduction in the mechanical performance of the composite material. In this work, a representative volume element (RVE) of a composite sub-laminate with a 90° ply discretized at micro-scale level, stacked within homogenized plies, is proposed to study the micro-residual stresses and the ply mechanical response considering the in-situ effect caused by the constraining adjacent layers. A model framework is developed using finite elements in Abaqus®/Standard with user-subroutines. The retrieved micro-residual stresses in the 90° layer are generated by the dissimilar chemical shrinkage and thermal expansions, plus the additional residual meso-scale stresses caused by the constraining effect of adjacent plies. The residual stresses in the constrained condition can achieve almost 80 % of the ply failure load for the 0/90/0 sub-laminate, meaning lower sub-laminate strain to failure. Thick laminates retrieve more residual stresses in the transverse 90° layer and exhibit lower constrained strength and more unstable post-failure response, demonstrating that thin-ply laminates exhibit beneficial constraining effects during the curing process.</description><subject>Finite element analysis (FEA)</subject><subject>Micro-mechanics</subject><subject>Polymer matrix composites (PMCs)</subject><subject>Residual/internal stress</subject><subject>Thermomechanical</subject><issn>0263-8223</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNqFkM1OwzAQhH0AiVJ4B79AUtv5M0eo-JOKuMDZsjdr6pI4lZ0icuLVcSgSR06r3dHMjj5CKGc5Z7xe7XIY-n0cwwHGXDBR5Jw3vJInZMFEXWRSiOKMnMe4Y4zJkvMF-XpyEIasR9hq70B3VHvdTdFFOlg6bpGitQjjvO27KV0cvHuMSfYUDsH5N9r_RASMrj2kgPQ_6Rip81RT0MEMfoX74XOic70huhFpp3vn9YgX5NTqLuLl71yS17vbl_VDtnm-f1xfbzIoajlmxpbCWFkZZplupS2xMFrWVtQVNGiEqNEKTGfbcFMJEGV51UiQNRQMWmOKJZHH3FQ1xoBW7YPrdZgUZ2qGp3bqD56a4akjvGS9OVox9ftwGFQEhx6wdSGRUe3g_g_5Blm0hHQ</recordid><startdate>20230901</startdate><enddate>20230901</enddate><creator>Goncalves, Paulo Teixeira</creator><creator>Arteiro, Albertino</creator><creator>Rocha, Nuno</creator><general>Elsevier Ltd</general><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0003-2427-0243</orcidid><orcidid>https://orcid.org/0000-0002-7779-2558</orcidid></search><sort><creationdate>20230901</creationdate><title>Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate</title><author>Goncalves, Paulo Teixeira ; Arteiro, Albertino ; Rocha, Nuno</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Finite element analysis (FEA)</topic><topic>Micro-mechanics</topic><topic>Polymer matrix composites (PMCs)</topic><topic>Residual/internal stress</topic><topic>Thermomechanical</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Goncalves, Paulo Teixeira</creatorcontrib><creatorcontrib>Arteiro, Albertino</creatorcontrib><creatorcontrib>Rocha, Nuno</creatorcontrib><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><jtitle>Composite structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Goncalves, Paulo Teixeira</au><au>Arteiro, Albertino</au><au>Rocha, Nuno</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate</atitle><jtitle>Composite structures</jtitle><date>2023-09-01</date><risdate>2023</risdate><volume>319</volume><spage>117158</spage><pages>117158-</pages><artnum>117158</artnum><issn>0263-8223</issn><abstract>•Micro-residual stresses reduce effective ply strength in constrained conditions.•Ply residual stresses can achieve more than 50 % of failure load.•Thick ply laminates tend to retrieve more ply residual stresses.•Thin ply laminate exhibits higher strength and lower crack opening after failure.
During the manufacturing of thermoset-based carbon fiber reinforced polymers (CFRPs), micro-residual stresses are developed in the material, due a mismatch of the chemical-thermal-mechanical properties of the fibers and the polymer matrix. This ultimately leads to a reduction in the mechanical performance of the composite material. In this work, a representative volume element (RVE) of a composite sub-laminate with a 90° ply discretized at micro-scale level, stacked within homogenized plies, is proposed to study the micro-residual stresses and the ply mechanical response considering the in-situ effect caused by the constraining adjacent layers. A model framework is developed using finite elements in Abaqus®/Standard with user-subroutines. The retrieved micro-residual stresses in the 90° layer are generated by the dissimilar chemical shrinkage and thermal expansions, plus the additional residual meso-scale stresses caused by the constraining effect of adjacent plies. The residual stresses in the constrained condition can achieve almost 80 % of the ply failure load for the 0/90/0 sub-laminate, meaning lower sub-laminate strain to failure. Thick laminates retrieve more residual stresses in the transverse 90° layer and exhibit lower constrained strength and more unstable post-failure response, demonstrating that thin-ply laminates exhibit beneficial constraining effects during the curing process.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.compstruct.2023.117158</doi><orcidid>https://orcid.org/0000-0003-2427-0243</orcidid><orcidid>https://orcid.org/0000-0002-7779-2558</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0263-8223 |
ispartof | Composite structures, 2023-09, Vol.319, p.117158, Article 117158 |
issn | 0263-8223 |
language | eng |
recordid | cdi_crossref_primary_10_1016_j_compstruct_2023_117158 |
source | ScienceDirect Journals |
subjects | Finite element analysis (FEA) Micro-mechanics Polymer matrix composites (PMCs) Residual/internal stress Thermomechanical |
title | Micro-mechanical analysis of the effect of ply thickness on curing micro-residual stresses in a carbon/epoxy composite laminate |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T02%3A42%3A27IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-elsevier_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Micro-mechanical%20analysis%20of%20the%20effect%20of%20ply%20thickness%20on%20curing%20micro-residual%20stresses%20in%20a%20carbon/epoxy%20composite%20laminate&rft.jtitle=Composite%20structures&rft.au=Goncalves,%20Paulo%20Teixeira&rft.date=2023-09-01&rft.volume=319&rft.spage=117158&rft.pages=117158-&rft.artnum=117158&rft.issn=0263-8223&rft_id=info:doi/10.1016/j.compstruct.2023.117158&rft_dat=%3Celsevier_cross%3ES0263822323005020%3C/elsevier_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c368t-bf42bf85b0f0ad8f4e3ba86f265c7eb226ef2ef4ef71b52c244978c86c30cdbb3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |