Loading…
A viscoelastic in-plane damage model for fibrous composite materials
This work presents a viscoelastic in-plane damage model for fibrous composites. The material behavior is modeled as linear viscoelastic, with brittle failure in the fiber-dominated direction, and progressive degradation of the matrix-dominated properties, when the composite is loaded perpendicularly...
Saved in:
Published in: | Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications Journal of materials, design and applications, 2022-07, Vol.236 (7), p.1364-1378 |
---|---|
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-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753 |
---|---|
cites | cdi_FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753 |
container_end_page | 1378 |
container_issue | 7 |
container_start_page | 1364 |
container_title | Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications |
container_volume | 236 |
creator | Quirino, Matheus Urzedo Tita, Volnei Ribeiro, Marcelo Leite |
description | This work presents a viscoelastic in-plane damage model for fibrous composites. The material behavior is modeled as linear viscoelastic, with brittle failure in the fiber-dominated direction, and progressive degradation of the matrix-dominated properties, when the composite is loaded perpendicularly to the fibers or in in-plane shear. An evaluation procedure has been performed by comparing computational stress-strain curves against tensile tests curves under three different displacement rates. In addition, a calibration of the viscoelastic properties, by means of the response surface methodology, is also presented. The proposed material model has shown reasonable performance up to the material reaching an experimentally-verified modulus transition zone. Besides, the viscoelastic calibration procedure has produced a good agreement with the experimental results, concerning maximum stresses. It was observed that the computational stress-strain curve has deviated from the experimental one for higher stress values, indicating that it is necessary to improve the assessment of the nonlinear phenomena, which occur within the material. |
doi_str_mv | 10.1177/14644207211065090 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2682737872</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_14644207211065090</sage_id><sourcerecordid>2682737872</sourcerecordid><originalsourceid>FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753</originalsourceid><addsrcrecordid>eNp1UEtLxDAQDqLgWv0B3gKeu04e7WyPy_qEBS96Lmk6lSztpiZdwX9vygoexNM38D1m5mPsWsBSCMRboUutJaAUAsoCKjhhCwla5AqwPGWLmc9nwTm7iHEHAAIBF-xuzT9dtJ56EydnudvnY2_2xFszmHfig2-p550PvHNN8IfIrR9GH92UODNRcKaPl-ysS0BXP5ixt4f7181Tvn15fN6st7lVQk55IxVqpPlKpa3WBNTpSqKmVqpOl01RUlG0FhDaxlYSTCPThEoqUa2wUBm7OeaOwX8cKE71zh_CPq2sZbmSqHCVojMmjiobfIyBunoMbjDhqxZQz2XVf8pKnuXRE9PTv6n_G74B5UFnoA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2682737872</pqid></control><display><type>article</type><title>A viscoelastic in-plane damage model for fibrous composite materials</title><source>SAGE</source><source>IMechE Titles Via Sage</source><creator>Quirino, Matheus Urzedo ; Tita, Volnei ; Ribeiro, Marcelo Leite</creator><creatorcontrib>Quirino, Matheus Urzedo ; Tita, Volnei ; Ribeiro, Marcelo Leite</creatorcontrib><description>This work presents a viscoelastic in-plane damage model for fibrous composites. The material behavior is modeled as linear viscoelastic, with brittle failure in the fiber-dominated direction, and progressive degradation of the matrix-dominated properties, when the composite is loaded perpendicularly to the fibers or in in-plane shear. An evaluation procedure has been performed by comparing computational stress-strain curves against tensile tests curves under three different displacement rates. In addition, a calibration of the viscoelastic properties, by means of the response surface methodology, is also presented. The proposed material model has shown reasonable performance up to the material reaching an experimentally-verified modulus transition zone. Besides, the viscoelastic calibration procedure has produced a good agreement with the experimental results, concerning maximum stresses. It was observed that the computational stress-strain curve has deviated from the experimental one for higher stress values, indicating that it is necessary to improve the assessment of the nonlinear phenomena, which occur within the material.</description><identifier>ISSN: 1464-4207</identifier><identifier>EISSN: 2041-3076</identifier><identifier>DOI: 10.1177/14644207211065090</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Calibration ; Composite materials ; Damage assessment ; Fiber composites ; Nonlinear phenomena ; Response surface methodology ; Stress-strain curves ; Stress-strain relationships ; Tensile tests ; Viscoelasticity</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications, 2022-07, Vol.236 (7), p.1364-1378</ispartof><rights>IMechE 2021</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753</citedby><cites>FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753</cites><orcidid>0000-0003-2686-2920 ; 0000-0002-8199-1162 ; 0000-0002-5586-2500</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/14644207211065090$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/14644207211065090$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,780,784,21913,27924,27925,45059,45447,79364</link.rule.ids></links><search><creatorcontrib>Quirino, Matheus Urzedo</creatorcontrib><creatorcontrib>Tita, Volnei</creatorcontrib><creatorcontrib>Ribeiro, Marcelo Leite</creatorcontrib><title>A viscoelastic in-plane damage model for fibrous composite materials</title><title>Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications</title><addtitle>Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications</addtitle><description>This work presents a viscoelastic in-plane damage model for fibrous composites. The material behavior is modeled as linear viscoelastic, with brittle failure in the fiber-dominated direction, and progressive degradation of the matrix-dominated properties, when the composite is loaded perpendicularly to the fibers or in in-plane shear. An evaluation procedure has been performed by comparing computational stress-strain curves against tensile tests curves under three different displacement rates. In addition, a calibration of the viscoelastic properties, by means of the response surface methodology, is also presented. The proposed material model has shown reasonable performance up to the material reaching an experimentally-verified modulus transition zone. Besides, the viscoelastic calibration procedure has produced a good agreement with the experimental results, concerning maximum stresses. It was observed that the computational stress-strain curve has deviated from the experimental one for higher stress values, indicating that it is necessary to improve the assessment of the nonlinear phenomena, which occur within the material.</description><subject>Calibration</subject><subject>Composite materials</subject><subject>Damage assessment</subject><subject>Fiber composites</subject><subject>Nonlinear phenomena</subject><subject>Response surface methodology</subject><subject>Stress-strain curves</subject><subject>Stress-strain relationships</subject><subject>Tensile tests</subject><subject>Viscoelasticity</subject><issn>1464-4207</issn><issn>2041-3076</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1UEtLxDAQDqLgWv0B3gKeu04e7WyPy_qEBS96Lmk6lSztpiZdwX9vygoexNM38D1m5mPsWsBSCMRboUutJaAUAsoCKjhhCwla5AqwPGWLmc9nwTm7iHEHAAIBF-xuzT9dtJ56EydnudvnY2_2xFszmHfig2-p550PvHNN8IfIrR9GH92UODNRcKaPl-ysS0BXP5ixt4f7181Tvn15fN6st7lVQk55IxVqpPlKpa3WBNTpSqKmVqpOl01RUlG0FhDaxlYSTCPThEoqUa2wUBm7OeaOwX8cKE71zh_CPq2sZbmSqHCVojMmjiobfIyBunoMbjDhqxZQz2XVf8pKnuXRE9PTv6n_G74B5UFnoA</recordid><startdate>20220701</startdate><enddate>20220701</enddate><creator>Quirino, Matheus Urzedo</creator><creator>Tita, Volnei</creator><creator>Ribeiro, Marcelo Leite</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>JG9</scope><orcidid>https://orcid.org/0000-0003-2686-2920</orcidid><orcidid>https://orcid.org/0000-0002-8199-1162</orcidid><orcidid>https://orcid.org/0000-0002-5586-2500</orcidid></search><sort><creationdate>20220701</creationdate><title>A viscoelastic in-plane damage model for fibrous composite materials</title><author>Quirino, Matheus Urzedo ; Tita, Volnei ; Ribeiro, Marcelo Leite</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Calibration</topic><topic>Composite materials</topic><topic>Damage assessment</topic><topic>Fiber composites</topic><topic>Nonlinear phenomena</topic><topic>Response surface methodology</topic><topic>Stress-strain curves</topic><topic>Stress-strain relationships</topic><topic>Tensile tests</topic><topic>Viscoelasticity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Quirino, Matheus Urzedo</creatorcontrib><creatorcontrib>Tita, Volnei</creatorcontrib><creatorcontrib>Ribeiro, Marcelo Leite</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Quirino, Matheus Urzedo</au><au>Tita, Volnei</au><au>Ribeiro, Marcelo Leite</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A viscoelastic in-plane damage model for fibrous composite materials</atitle><jtitle>Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications</jtitle><addtitle>Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications</addtitle><date>2022-07-01</date><risdate>2022</risdate><volume>236</volume><issue>7</issue><spage>1364</spage><epage>1378</epage><pages>1364-1378</pages><issn>1464-4207</issn><eissn>2041-3076</eissn><abstract>This work presents a viscoelastic in-plane damage model for fibrous composites. The material behavior is modeled as linear viscoelastic, with brittle failure in the fiber-dominated direction, and progressive degradation of the matrix-dominated properties, when the composite is loaded perpendicularly to the fibers or in in-plane shear. An evaluation procedure has been performed by comparing computational stress-strain curves against tensile tests curves under three different displacement rates. In addition, a calibration of the viscoelastic properties, by means of the response surface methodology, is also presented. The proposed material model has shown reasonable performance up to the material reaching an experimentally-verified modulus transition zone. Besides, the viscoelastic calibration procedure has produced a good agreement with the experimental results, concerning maximum stresses. It was observed that the computational stress-strain curve has deviated from the experimental one for higher stress values, indicating that it is necessary to improve the assessment of the nonlinear phenomena, which occur within the material.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/14644207211065090</doi><tpages>15</tpages><orcidid>https://orcid.org/0000-0003-2686-2920</orcidid><orcidid>https://orcid.org/0000-0002-8199-1162</orcidid><orcidid>https://orcid.org/0000-0002-5586-2500</orcidid></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1464-4207 |
ispartof | Proceedings of the Institution of Mechanical Engineers. Part L, Journal of materials, design and applications, 2022-07, Vol.236 (7), p.1364-1378 |
issn | 1464-4207 2041-3076 |
language | eng |
recordid | cdi_proquest_journals_2682737872 |
source | SAGE; IMechE Titles Via Sage |
subjects | Calibration Composite materials Damage assessment Fiber composites Nonlinear phenomena Response surface methodology Stress-strain curves Stress-strain relationships Tensile tests Viscoelasticity |
title | A viscoelastic in-plane damage model for fibrous composite materials |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T13%3A15%3A41IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20viscoelastic%20in-plane%20damage%20model%20for%20fibrous%20composite%20materials&rft.jtitle=Proceedings%20of%20the%20Institution%20of%20Mechanical%20Engineers.%20Part%20L,%20Journal%20of%20materials,%20design%20and%20applications&rft.au=Quirino,%20Matheus%20Urzedo&rft.date=2022-07-01&rft.volume=236&rft.issue=7&rft.spage=1364&rft.epage=1378&rft.pages=1364-1378&rft.issn=1464-4207&rft.eissn=2041-3076&rft_id=info:doi/10.1177/14644207211065090&rft_dat=%3Cproquest_cross%3E2682737872%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c312t-b23747e207234c44e0ef49274ed23f46b56e55dc070dbc920ab20db7323198753%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2682737872&rft_id=info:pmid/&rft_sage_id=10.1177_14644207211065090&rfr_iscdi=true |