Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method

A method for the probabilistic failure analysis of laminated composite plates with random system parameters subject to transverse loads is presented. System parameters such as material properties, plate thickness, and lamina strengths of a laminated composite plate are treated as baseline random var...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of engineering mechanics 2000-08, Vol.126 (8), p.812-820
Hauptverfasser: Lin, S. C, Kam, T. Y
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 820
container_issue 8
container_start_page 812
container_title Journal of engineering mechanics
container_volume 126
creator Lin, S. C
Kam, T. Y
description A method for the probabilistic failure analysis of laminated composite plates with random system parameters subject to transverse loads is presented. System parameters such as material properties, plate thickness, and lamina strengths of a laminated composite plate are treated as baseline random variables. The statistics of the baseline random variables obtained from experiments are used in a stochastic finite-element analysis for computing the statistical moments of stresses in the laminated composite plate. An appropriate failure criterion from which the statistical moments of first-ply failure load are derived via a first-order second moment method is used to construct the limit state equation of the plate in the probabilistic failure analysis. The reliability of the laminated plate is then computed using an assumed probability distribution function of the first-ply failure load. The feasibility and accuracy of the present method are validated by the experimental data of centrally loaded laminated composite plates with different layups. The suitability of several commonly used failure criteria for reliability analysis of laminated composite plates is also investigated by means of several examples.
doi_str_mv 10.1061/(ASCE)0733-9399(2000)126:8(812)
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_27660978</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>27660978</sourcerecordid><originalsourceid>FETCH-LOGICAL-a409t-fefc15b5d54b5def1ca4349667c3c08b2867c2da16852b0c2bb4fde880f5d2a73</originalsourceid><addsrcrecordid>eNp9kF2LEzEUhoMoWFf_Qy5E24tZk8xMJuOFUGq7Kq27sF3wLmTyoVkyk5ozVfrvzdhV7wwkeQkPbw4PQq8puaSE0zfz5e1qvSBNWRZt2bZzRghZUMbfirmgbPEIzWhblUUjRPsYzf5yT9EzgHtCaMVbPkM_b1LsVOeDh9FrvFE-HJPFy0GFE3jA0eF9UgP8sAlsOOFtVMYavFW9H9SY0yr2hwh-tPgm5AfAd-CHr3jjE4zFdTI24Vur42DwLvZ2GPHOjt-ieY6eOBXAvni4L9DdZr1ffSi211cfV8ttoSrSjoWzTtO6q01d5cM6qlVVVi3njS41ER0TOTGjKBc164hmXVc5Y4UgrjZMNeUFenXuPaT4_WhhlL0HbUNQg41HkKzhnLSNyOC7M6hTBEjWyUPyvUonSYmchEs5CZeTSDmJlJNwmYVLIbPwXPDy4ScFWgWXrWkP_1oqVjNSZ-zLGcuUlffxmLJqkJ_Wn3fv97kxF5JpiWlT9jvTPyP8f4Jfr4CbpA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27660978</pqid></control><display><type>article</type><title>Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method</title><source>American Society of Civil Engineers:NESLI2:Journals:2014</source><creator>Lin, S. C ; Kam, T. Y</creator><creatorcontrib>Lin, S. C ; Kam, T. Y</creatorcontrib><description>A method for the probabilistic failure analysis of laminated composite plates with random system parameters subject to transverse loads is presented. System parameters such as material properties, plate thickness, and lamina strengths of a laminated composite plate are treated as baseline random variables. The statistics of the baseline random variables obtained from experiments are used in a stochastic finite-element analysis for computing the statistical moments of stresses in the laminated composite plate. An appropriate failure criterion from which the statistical moments of first-ply failure load are derived via a first-order second moment method is used to construct the limit state equation of the plate in the probabilistic failure analysis. The reliability of the laminated plate is then computed using an assumed probability distribution function of the first-ply failure load. The feasibility and accuracy of the present method are validated by the experimental data of centrally loaded laminated composite plates with different layups. The suitability of several commonly used failure criteria for reliability analysis of laminated composite plates is also investigated by means of several examples.</description><identifier>ISSN: 0733-9399</identifier><identifier>EISSN: 1943-7889</identifier><identifier>DOI: 10.1061/(ASCE)0733-9399(2000)126:8(812)</identifier><identifier>CODEN: JENMDT</identifier><language>eng</language><publisher>Reston, VA: American Society of Civil Engineers</publisher><subject>Applied sciences ; Composites ; Exact sciences and technology ; Forms of application and semi-finished materials ; Fracture mechanics (crack, fatigue, damage...) ; Fracture mechanics, fatigue and cracks ; Fundamental areas of phenomenology (including applications) ; Physics ; Polymer industry, paints, wood ; Solid mechanics ; Structural and continuum mechanics ; TECHNICAL PAPERS ; Technology of polymers</subject><ispartof>Journal of engineering mechanics, 2000-08, Vol.126 (8), p.812-820</ispartof><rights>2000 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a409t-fefc15b5d54b5def1ca4349667c3c08b2867c2da16852b0c2bb4fde880f5d2a73</citedby><cites>FETCH-LOGICAL-a409t-fefc15b5d54b5def1ca4349667c3c08b2867c2da16852b0c2bb4fde880f5d2a73</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttp://ascelibrary.org/doi/pdf/10.1061/(ASCE)0733-9399(2000)126:8(812)$$EPDF$$P50$$Gasce$$H</linktopdf><linktohtml>$$Uhttp://ascelibrary.org/doi/abs/10.1061/(ASCE)0733-9399(2000)126:8(812)$$EHTML$$P50$$Gasce$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,75936,75944</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=1425205$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Lin, S. C</creatorcontrib><creatorcontrib>Kam, T. Y</creatorcontrib><title>Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method</title><title>Journal of engineering mechanics</title><description>A method for the probabilistic failure analysis of laminated composite plates with random system parameters subject to transverse loads is presented. System parameters such as material properties, plate thickness, and lamina strengths of a laminated composite plate are treated as baseline random variables. The statistics of the baseline random variables obtained from experiments are used in a stochastic finite-element analysis for computing the statistical moments of stresses in the laminated composite plate. An appropriate failure criterion from which the statistical moments of first-ply failure load are derived via a first-order second moment method is used to construct the limit state equation of the plate in the probabilistic failure analysis. The reliability of the laminated plate is then computed using an assumed probability distribution function of the first-ply failure load. The feasibility and accuracy of the present method are validated by the experimental data of centrally loaded laminated composite plates with different layups. The suitability of several commonly used failure criteria for reliability analysis of laminated composite plates is also investigated by means of several examples.</description><subject>Applied sciences</subject><subject>Composites</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Fracture mechanics (crack, fatigue, damage...)</subject><subject>Fracture mechanics, fatigue and cracks</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Polymer industry, paints, wood</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>TECHNICAL PAPERS</subject><subject>Technology of polymers</subject><issn>0733-9399</issn><issn>1943-7889</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2000</creationdate><recordtype>article</recordtype><recordid>eNp9kF2LEzEUhoMoWFf_Qy5E24tZk8xMJuOFUGq7Kq27sF3wLmTyoVkyk5ozVfrvzdhV7wwkeQkPbw4PQq8puaSE0zfz5e1qvSBNWRZt2bZzRghZUMbfirmgbPEIzWhblUUjRPsYzf5yT9EzgHtCaMVbPkM_b1LsVOeDh9FrvFE-HJPFy0GFE3jA0eF9UgP8sAlsOOFtVMYavFW9H9SY0yr2hwh-tPgm5AfAd-CHr3jjE4zFdTI24Vur42DwLvZ2GPHOjt-ieY6eOBXAvni4L9DdZr1ffSi211cfV8ttoSrSjoWzTtO6q01d5cM6qlVVVi3njS41ER0TOTGjKBc164hmXVc5Y4UgrjZMNeUFenXuPaT4_WhhlL0HbUNQg41HkKzhnLSNyOC7M6hTBEjWyUPyvUonSYmchEs5CZeTSDmJlJNwmYVLIbPwXPDy4ScFWgWXrWkP_1oqVjNSZ-zLGcuUlffxmLJqkJ_Wn3fv97kxF5JpiWlT9jvTPyP8f4Jfr4CbpA</recordid><startdate>20000801</startdate><enddate>20000801</enddate><creator>Lin, S. C</creator><creator>Kam, T. Y</creator><general>American Society of Civil Engineers</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope></search><sort><creationdate>20000801</creationdate><title>Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method</title><author>Lin, S. C ; Kam, T. Y</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a409t-fefc15b5d54b5def1ca4349667c3c08b2867c2da16852b0c2bb4fde880f5d2a73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2000</creationdate><topic>Applied sciences</topic><topic>Composites</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Fracture mechanics (crack, fatigue, damage...)</topic><topic>Fracture mechanics, fatigue and cracks</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Polymer industry, paints, wood</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>TECHNICAL PAPERS</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lin, S. C</creatorcontrib><creatorcontrib>Kam, T. Y</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of engineering mechanics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lin, S. C</au><au>Kam, T. Y</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method</atitle><jtitle>Journal of engineering mechanics</jtitle><date>2000-08-01</date><risdate>2000</risdate><volume>126</volume><issue>8</issue><spage>812</spage><epage>820</epage><pages>812-820</pages><issn>0733-9399</issn><eissn>1943-7889</eissn><coden>JENMDT</coden><abstract>A method for the probabilistic failure analysis of laminated composite plates with random system parameters subject to transverse loads is presented. System parameters such as material properties, plate thickness, and lamina strengths of a laminated composite plate are treated as baseline random variables. The statistics of the baseline random variables obtained from experiments are used in a stochastic finite-element analysis for computing the statistical moments of stresses in the laminated composite plate. An appropriate failure criterion from which the statistical moments of first-ply failure load are derived via a first-order second moment method is used to construct the limit state equation of the plate in the probabilistic failure analysis. The reliability of the laminated plate is then computed using an assumed probability distribution function of the first-ply failure load. The feasibility and accuracy of the present method are validated by the experimental data of centrally loaded laminated composite plates with different layups. The suitability of several commonly used failure criteria for reliability analysis of laminated composite plates is also investigated by means of several examples.</abstract><cop>Reston, VA</cop><pub>American Society of Civil Engineers</pub><doi>10.1061/(ASCE)0733-9399(2000)126:8(812)</doi><tpages>9</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0733-9399
ispartof Journal of engineering mechanics, 2000-08, Vol.126 (8), p.812-820
issn 0733-9399
1943-7889
language eng
recordid cdi_proquest_miscellaneous_27660978
source American Society of Civil Engineers:NESLI2:Journals:2014
subjects Applied sciences
Composites
Exact sciences and technology
Forms of application and semi-finished materials
Fracture mechanics (crack, fatigue, damage...)
Fracture mechanics, fatigue and cracks
Fundamental areas of phenomenology (including applications)
Physics
Polymer industry, paints, wood
Solid mechanics
Structural and continuum mechanics
TECHNICAL PAPERS
Technology of polymers
title Probabilistic Failure Analysis of Transversely Loaded Laminated Composite Plates Using First-Order Second Moment Method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T19%3A18%3A01IST&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=Probabilistic%20Failure%20Analysis%20of%20Transversely%20Loaded%20Laminated%20Composite%20Plates%20Using%20First-Order%20Second%20Moment%20Method&rft.jtitle=Journal%20of%20engineering%20mechanics&rft.au=Lin,%20S.%20C&rft.date=2000-08-01&rft.volume=126&rft.issue=8&rft.spage=812&rft.epage=820&rft.pages=812-820&rft.issn=0733-9399&rft.eissn=1943-7889&rft.coden=JENMDT&rft_id=info:doi/10.1061/(ASCE)0733-9399(2000)126:8(812)&rft_dat=%3Cproquest_cross%3E27660978%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=27660978&rft_id=info:pmid/&rfr_iscdi=true