Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element

Stiffened plates are used in several applications, such as aircrafts, ships, and aerospace structures. Dynamic analysis of stiffened and unstiffened composite laminated plate is presented in this work using a high-order finite element. The shear effect has been taken into consideration in the deriva...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of composite materials 2010-02, Vol.44 (3), p.327-346
1. Verfasser: Hegaze, Moutaz M.
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 346
container_issue 3
container_start_page 327
container_title Journal of composite materials
container_volume 44
creator Hegaze, Moutaz M.
description Stiffened plates are used in several applications, such as aircrafts, ships, and aerospace structures. Dynamic analysis of stiffened and unstiffened composite laminated plate is presented in this work using a high-order finite element. The shear effect has been taken into consideration in the derivation of the element. This technique gives us the ability to avoid the problem of unsymmetry of stiffness matrix due to large deformation effect. The accuracy of the proposed derivation of the element has been verified through the comparison of the results with published, software (ANSYS-11) and experimental results. The effects of the number of layers and degree of orthtropy are studied with different case studies by different boundary conditions and thickness-to-span ratio. A comparison with different kind of elements is presented.
doi_str_mv 10.1177/0021998309345356
format Article
fullrecord <record><control><sourceid>sage_cross</sourceid><recordid>TN_cdi_crossref_primary_10_1177_0021998309345356</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0021998309345356</sage_id><sourcerecordid>10.1177_0021998309345356</sourcerecordid><originalsourceid>FETCH-LOGICAL-c311t-b27421590f88ca43dc581c56bcabf999cfd7958282a078cced0a4d873f9ef8a93</originalsourceid><addsrcrecordid>eNp1kDtPwzAUhS0EEqWwM3phDPiR1PZYldIiVYAEldiiW8curhKn8g1D_z2JijogMd3H-c4ZDiG3nN1zrtQDY4IboyUzMi9kMTkjI15IlikjP8_JaJCzQb8kV4g7xpji-WREmpc21iE6SPTxEKEJlk4j1AcMSFtP37vgvYuuohAruo54ulc9G6Hrt1nb7FsMnaNvdf9AusYQtxToMmy_sjZVLtF57RoXu2ty4aFGd_M7x2T9NP-YLbPV6-J5Nl1lVnLeZRuhcsELw7zWFnJZ2UJzW0w2FjbeGGN9pUyhhRbAlLbWVQzySivpjfMajBwTdsy1qUVMzpf7FBpIh5Kzcqir_FtXb7k7WvaAFmqfINqAJ58QMu_pgcuOHMLWlbv2O_V14f-5P8Y2eEg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element</title><source>SAGE Complete</source><creator>Hegaze, Moutaz M.</creator><creatorcontrib>Hegaze, Moutaz M.</creatorcontrib><description>Stiffened plates are used in several applications, such as aircrafts, ships, and aerospace structures. Dynamic analysis of stiffened and unstiffened composite laminated plate is presented in this work using a high-order finite element. The shear effect has been taken into consideration in the derivation of the element. This technique gives us the ability to avoid the problem of unsymmetry of stiffness matrix due to large deformation effect. The accuracy of the proposed derivation of the element has been verified through the comparison of the results with published, software (ANSYS-11) and experimental results. The effects of the number of layers and degree of orthtropy are studied with different case studies by different boundary conditions and thickness-to-span ratio. A comparison with different kind of elements is presented.</description><identifier>ISSN: 0021-9983</identifier><identifier>EISSN: 1530-793X</identifier><identifier>DOI: 10.1177/0021998309345356</identifier><identifier>CODEN: JCOMBI</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Applied sciences ; Exact sciences and technology ; Fundamental areas of phenomenology (including applications) ; Ground, air and sea transportation, marine construction ; Marine construction ; Physics ; Solid mechanics ; Structural and continuum mechanics ; Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><ispartof>Journal of composite materials, 2010-02, Vol.44 (3), p.327-346</ispartof><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c311t-b27421590f88ca43dc581c56bcabf999cfd7958282a078cced0a4d873f9ef8a93</citedby><cites>FETCH-LOGICAL-c311t-b27421590f88ca43dc581c56bcabf999cfd7958282a078cced0a4d873f9ef8a93</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0021998309345356$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0021998309345356$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21798,27901,27902,43597,43598</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=22348306$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Hegaze, Moutaz M.</creatorcontrib><title>Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element</title><title>Journal of composite materials</title><description>Stiffened plates are used in several applications, such as aircrafts, ships, and aerospace structures. Dynamic analysis of stiffened and unstiffened composite laminated plate is presented in this work using a high-order finite element. The shear effect has been taken into consideration in the derivation of the element. This technique gives us the ability to avoid the problem of unsymmetry of stiffness matrix due to large deformation effect. The accuracy of the proposed derivation of the element has been verified through the comparison of the results with published, software (ANSYS-11) and experimental results. The effects of the number of layers and degree of orthtropy are studied with different case studies by different boundary conditions and thickness-to-span ratio. A comparison with different kind of elements is presented.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Ground, air and sea transportation, marine construction</subject><subject>Marine construction</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><issn>0021-9983</issn><issn>1530-793X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNp1kDtPwzAUhS0EEqWwM3phDPiR1PZYldIiVYAEldiiW8curhKn8g1D_z2JijogMd3H-c4ZDiG3nN1zrtQDY4IboyUzMi9kMTkjI15IlikjP8_JaJCzQb8kV4g7xpji-WREmpc21iE6SPTxEKEJlk4j1AcMSFtP37vgvYuuohAruo54ulc9G6Hrt1nb7FsMnaNvdf9AusYQtxToMmy_sjZVLtF57RoXu2ty4aFGd_M7x2T9NP-YLbPV6-J5Nl1lVnLeZRuhcsELw7zWFnJZ2UJzW0w2FjbeGGN9pUyhhRbAlLbWVQzySivpjfMajBwTdsy1qUVMzpf7FBpIh5Kzcqir_FtXb7k7WvaAFmqfINqAJ58QMu_pgcuOHMLWlbv2O_V14f-5P8Y2eEg</recordid><startdate>20100201</startdate><enddate>20100201</enddate><creator>Hegaze, Moutaz M.</creator><general>SAGE Publications</general><general>Sage Publications</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20100201</creationdate><title>Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element</title><author>Hegaze, Moutaz M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c311t-b27421590f88ca43dc581c56bcabf999cfd7958282a078cced0a4d873f9ef8a93</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2010</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Ground, air and sea transportation, marine construction</topic><topic>Marine construction</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hegaze, Moutaz M.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hegaze, Moutaz M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element</atitle><jtitle>Journal of composite materials</jtitle><date>2010-02-01</date><risdate>2010</risdate><volume>44</volume><issue>3</issue><spage>327</spage><epage>346</epage><pages>327-346</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><coden>JCOMBI</coden><abstract>Stiffened plates are used in several applications, such as aircrafts, ships, and aerospace structures. Dynamic analysis of stiffened and unstiffened composite laminated plate is presented in this work using a high-order finite element. The shear effect has been taken into consideration in the derivation of the element. This technique gives us the ability to avoid the problem of unsymmetry of stiffness matrix due to large deformation effect. The accuracy of the proposed derivation of the element has been verified through the comparison of the results with published, software (ANSYS-11) and experimental results. The effects of the number of layers and degree of orthtropy are studied with different case studies by different boundary conditions and thickness-to-span ratio. A comparison with different kind of elements is presented.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0021998309345356</doi><tpages>20</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0021-9983
ispartof Journal of composite materials, 2010-02, Vol.44 (3), p.327-346
issn 0021-9983
1530-793X
language eng
recordid cdi_crossref_primary_10_1177_0021998309345356
source SAGE Complete
subjects Applied sciences
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Ground, air and sea transportation, marine construction
Marine construction
Physics
Solid mechanics
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
title Nonlinear Dynamic Analysis of Stiffened and Unstiffened Laminated Composite Plates Using a High-order Element
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-21T18%3A36%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-sage_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Nonlinear%20Dynamic%20Analysis%20of%20Stiffened%20and%20Unstiffened%20Laminated%20Composite%20Plates%20Using%20a%20High-order%20Element&rft.jtitle=Journal%20of%20composite%20materials&rft.au=Hegaze,%20Moutaz%20M.&rft.date=2010-02-01&rft.volume=44&rft.issue=3&rft.spage=327&rft.epage=346&rft.pages=327-346&rft.issn=0021-9983&rft.eissn=1530-793X&rft.coden=JCOMBI&rft_id=info:doi/10.1177/0021998309345356&rft_dat=%3Csage_cross%3E10.1177_0021998309345356%3C/sage_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_sage_id=10.1177_0021998309345356&rfr_iscdi=true