Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations

Two related criteria based on stress distribution are presented for predicting the uniaxial tensile strength of laminated composites containing through the thickness discontinuities of a general shape. The criteria result in two parameter (unnotched tensile strength and a characteristic dimension) m...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of composite materials 1974-07, Vol.8 (3), p.253-265
Hauptverfasser: Whitney, J.M., Nuismer, R.J.
Format: Artikel
Sprache:eng
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 265
container_issue 3
container_start_page 253
container_title Journal of composite materials
container_volume 8
creator Whitney, J.M.
Nuismer, R.J.
description Two related criteria based on stress distribution are presented for predicting the uniaxial tensile strength of laminated composites containing through the thickness discontinuities of a general shape. The criteria result in two parameter (unnotched tensile strength and a characteristic dimension) models which are capable of predicting observed discontinuity size effects without resorting to classical concepts of linear elastic fracture mechanics. As a direct consequence of the stress criteria, however, a relationship between Mode I fracture toughness and unnotched laminate tensile strength is determined. Limited comparison of theory to experimental data for circular holes and straight cracks yields good results. The simplicity of the analytical approach coupled with its generality make it of practical value to the designer.
doi_str_mv 10.1177/002199837400800303
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_33609687</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_002199837400800303</sage_id><sourcerecordid>33609687</sourcerecordid><originalsourceid>FETCH-LOGICAL-c413t-2019f46f56a736d9271e3fff5ae2c2050c688db04f66d095529e826d5fc3dc93</originalsourceid><addsrcrecordid>eNqFkMFKAzEQhoMoWKsv4GlP3tZOkk2yOcpiVSgI2oO3ELNJSekmNckefHu3tDdBTzPMfN_A_AjdYrjHWIgFAMFStlQ0AC0ABXqGZphRqIWkH-dodgDqA3GJrnLeAoDADZ-ht_eSbM7VMmlTxmSrLvlik9eVi6la6cEHXWxfdXHYxzyt8tSGon3wYVOd5GlibChJFx9DvkYXTu-yvTnVOVovH9fdc716fXrpHla1aTAtNQEsXcMd41pQ3ksisKXOOaYtMQQYGN62_Sc0jvMeJGNE2pbwnjlDeyPpHN0dz-5T_BptLmrw2djdTgcbx6wo5SB5K_4FCSGccIwnkBxBk2LOyTq1T37Q6VthUIeY1e-YJ2lxlLLeWLWNYwrT038ZP4JqfVs</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>22262611</pqid></control><display><type>article</type><title>Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations</title><source>SAGE Complete A-Z List</source><creator>Whitney, J.M. ; Nuismer, R.J.</creator><creatorcontrib>Whitney, J.M. ; Nuismer, R.J.</creatorcontrib><description>Two related criteria based on stress distribution are presented for predicting the uniaxial tensile strength of laminated composites containing through the thickness discontinuities of a general shape. The criteria result in two parameter (unnotched tensile strength and a characteristic dimension) models which are capable of predicting observed discontinuity size effects without resorting to classical concepts of linear elastic fracture mechanics. As a direct consequence of the stress criteria, however, a relationship between Mode I fracture toughness and unnotched laminate tensile strength is determined. Limited comparison of theory to experimental data for circular holes and straight cracks yields good results. The simplicity of the analytical approach coupled with its generality make it of practical value to the designer.</description><identifier>ISSN: 0021-9983</identifier><identifier>EISSN: 1530-793X</identifier><identifier>DOI: 10.1177/002199837400800303</identifier><language>eng</language><publisher>Thousand Oaks, CA: SAGE Publications</publisher><ispartof>Journal of composite materials, 1974-07, Vol.8 (3), p.253-265</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c413t-2019f46f56a736d9271e3fff5ae2c2050c688db04f66d095529e826d5fc3dc93</citedby><cites>FETCH-LOGICAL-c413t-2019f46f56a736d9271e3fff5ae2c2050c688db04f66d095529e826d5fc3dc93</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/002199837400800303$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/002199837400800303$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,778,782,21802,27907,27908,43604,43605</link.rule.ids></links><search><creatorcontrib>Whitney, J.M.</creatorcontrib><creatorcontrib>Nuismer, R.J.</creatorcontrib><title>Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations</title><title>Journal of composite materials</title><description>Two related criteria based on stress distribution are presented for predicting the uniaxial tensile strength of laminated composites containing through the thickness discontinuities of a general shape. The criteria result in two parameter (unnotched tensile strength and a characteristic dimension) models which are capable of predicting observed discontinuity size effects without resorting to classical concepts of linear elastic fracture mechanics. As a direct consequence of the stress criteria, however, a relationship between Mode I fracture toughness and unnotched laminate tensile strength is determined. Limited comparison of theory to experimental data for circular holes and straight cracks yields good results. The simplicity of the analytical approach coupled with its generality make it of practical value to the designer.</description><issn>0021-9983</issn><issn>1530-793X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1974</creationdate><recordtype>article</recordtype><recordid>eNqFkMFKAzEQhoMoWKsv4GlP3tZOkk2yOcpiVSgI2oO3ELNJSekmNckefHu3tDdBTzPMfN_A_AjdYrjHWIgFAMFStlQ0AC0ABXqGZphRqIWkH-dodgDqA3GJrnLeAoDADZ-ht_eSbM7VMmlTxmSrLvlik9eVi6la6cEHXWxfdXHYxzyt8tSGon3wYVOd5GlibChJFx9DvkYXTu-yvTnVOVovH9fdc716fXrpHla1aTAtNQEsXcMd41pQ3ksisKXOOaYtMQQYGN62_Sc0jvMeJGNE2pbwnjlDeyPpHN0dz-5T_BptLmrw2djdTgcbx6wo5SB5K_4FCSGccIwnkBxBk2LOyTq1T37Q6VthUIeY1e-YJ2lxlLLeWLWNYwrT038ZP4JqfVs</recordid><startdate>197407</startdate><enddate>197407</enddate><creator>Whitney, J.M.</creator><creator>Nuismer, R.J.</creator><general>SAGE Publications</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7SR</scope><scope>JG9</scope></search><sort><creationdate>197407</creationdate><title>Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations</title><author>Whitney, J.M. ; Nuismer, R.J.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c413t-2019f46f56a736d9271e3fff5ae2c2050c688db04f66d095529e826d5fc3dc93</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1974</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Whitney, J.M.</creatorcontrib><creatorcontrib>Nuismer, R.J.</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Engineered Materials Abstracts</collection><collection>Materials Research Database</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Whitney, J.M.</au><au>Nuismer, R.J.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations</atitle><jtitle>Journal of composite materials</jtitle><date>1974-07</date><risdate>1974</risdate><volume>8</volume><issue>3</issue><spage>253</spage><epage>265</epage><pages>253-265</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><abstract>Two related criteria based on stress distribution are presented for predicting the uniaxial tensile strength of laminated composites containing through the thickness discontinuities of a general shape. The criteria result in two parameter (unnotched tensile strength and a characteristic dimension) models which are capable of predicting observed discontinuity size effects without resorting to classical concepts of linear elastic fracture mechanics. As a direct consequence of the stress criteria, however, a relationship between Mode I fracture toughness and unnotched laminate tensile strength is determined. Limited comparison of theory to experimental data for circular holes and straight cracks yields good results. The simplicity of the analytical approach coupled with its generality make it of practical value to the designer.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/002199837400800303</doi><tpages>13</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0021-9983
ispartof Journal of composite materials, 1974-07, Vol.8 (3), p.253-265
issn 0021-9983
1530-793X
language eng
recordid cdi_proquest_miscellaneous_33609687
source SAGE Complete A-Z List
title Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T22%3A07%3A25IST&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=Stress%20Fracture%20Criteria%20for%20Laminated%20Composites%20Containing%20Stress%20Concentrations&rft.jtitle=Journal%20of%20composite%20materials&rft.au=Whitney,%20J.M.&rft.date=1974-07&rft.volume=8&rft.issue=3&rft.spage=253&rft.epage=265&rft.pages=253-265&rft.issn=0021-9983&rft.eissn=1530-793X&rft_id=info:doi/10.1177/002199837400800303&rft_dat=%3Cproquest_cross%3E33609687%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=22262611&rft_id=info:pmid/&rft_sage_id=10.1177_002199837400800303&rfr_iscdi=true