FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH

FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH

This research paper presents a higher order isogeometric laminated composite plate finite element formulation. The isogeometric formulation is based on NURBS (non-uniform rational B-splines) basis functions of varying degree. Plate kinematics is based on the third order shear deformation theory (TSD...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of Theoretical and Applied Mechanics (Warsaw) 2015-01, Vol.53 (2), p.453-466
Hauptverfasser: Peković, Ognjen, Stupar, Slobodan, Simonović, Aleksandar, Svorcan, Jelena, Trivković, Srdan
Format: Artikel
Sprache:eng
Schlagworte:
Buckling
Composite structures
Computational efficiency
Finite element method
Free vibration
Mathematical analysis
Mathematical models
Plates (structural members)
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 466
container_issue 2
container_start_page 453
container_title Journal of Theoretical and Applied Mechanics (Warsaw)
container_volume 53
creator Peković, Ognjen
Stupar, Slobodan
Simonović, Aleksandar
Svorcan, Jelena
Trivković, Srdan
description This research paper presents a higher order isogeometric laminated composite plate finite element formulation. The isogeometric formulation is based on NURBS (non-uniform rational B-splines) basis functions of varying degree. Plate kinematics is based on the third order shear deformation theory (TSDT) of Reddy in order to avoid shear locking. Free vibration and the buckling response of laminated composite plates are obtained and efficiency of the method is considered. Numerical results with different element order are presented and the obtained results are compared to analytical and conventional numerical results as well as existing isogeometric plate finite elements.
doi_str_mv 10.15632/jtam-pl.53.2.453
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1762079646</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>1762079646</sourcerecordid><originalsourceid>FETCH-LOGICAL-c278t-b4d2e7b556fdc47806a6ca022ad8fb61232616acf09b9900b5d1161386bec9b23</originalsourceid><addsrcrecordid>eNotkD1vgzAURRlaqVGaH9DNYxeoP7CBkRAHrBKMgFTqZJkvKRFpKE6G_vuSpst9uk_nveFY1guCDqKM4LfjRZ_scXAocbDjUvJgLZCLAxsHlD5ZK2OOEELsUxYQuLDO24Jz8CHWRVgJmYEw24D1PnpPRRbPJUw_S1ECuQWJiBNeAFls5kzDncjCim9AJHe5LEXFQZ7OixLsy9tllXAgShlzueNVISIQ5nkhwyh5th57PZhu9T-X1n7LqyixUxmLKEztBnv-xa7dFndeTSnr28b1fMg0azTEWLd-XzOECWaI6aaHQR0EENa0RYgh4rO6a4Iak6X1ev87Tufva2cu6nQwTTcM-qs7X41CHsPQC5jLZhTd0WY6GzN1vRqnw0lPPwpB9edU3ZyqcVCUKKxmp-QXkhhkIA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1762079646</pqid></control><display><type>article</type><title>FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH</title><source>Alma/SFX Local Collection</source><creator>Peković, Ognjen ; Stupar, Slobodan ; Simonović, Aleksandar ; Svorcan, Jelena ; Trivković, Srdan</creator><creatorcontrib>Peković, Ognjen ; Stupar, Slobodan ; Simonović, Aleksandar ; Svorcan, Jelena ; Trivković, Srdan</creatorcontrib><description>This research paper presents a higher order isogeometric laminated composite plate finite element formulation. The isogeometric formulation is based on NURBS (non-uniform rational B-splines) basis functions of varying degree. Plate kinematics is based on the third order shear deformation theory (TSDT) of Reddy in order to avoid shear locking. Free vibration and the buckling response of laminated composite plates are obtained and efficiency of the method is considered. Numerical results with different element order are presented and the obtained results are compared to analytical and conventional numerical results as well as existing isogeometric plate finite elements.</description><identifier>ISSN: 1429-2955</identifier><identifier>DOI: 10.15632/jtam-pl.53.2.453</identifier><language>eng</language><subject>Buckling ; Composite structures ; Computational efficiency ; Finite element method ; Free vibration ; Mathematical analysis ; Mathematical models ; Plates (structural members)</subject><ispartof>Journal of Theoretical and Applied Mechanics (Warsaw), 2015-01, Vol.53 (2), p.453-466</ispartof><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c278t-b4d2e7b556fdc47806a6ca022ad8fb61232616acf09b9900b5d1161386bec9b23</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids></links><search><creatorcontrib>Peković, Ognjen</creatorcontrib><creatorcontrib>Stupar, Slobodan</creatorcontrib><creatorcontrib>Simonović, Aleksandar</creatorcontrib><creatorcontrib>Svorcan, Jelena</creatorcontrib><creatorcontrib>Trivković, Srdan</creatorcontrib><title>FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH</title><title>Journal of Theoretical and Applied Mechanics (Warsaw)</title><description>This research paper presents a higher order isogeometric laminated composite plate finite element formulation. The isogeometric formulation is based on NURBS (non-uniform rational B-splines) basis functions of varying degree. Plate kinematics is based on the third order shear deformation theory (TSDT) of Reddy in order to avoid shear locking. Free vibration and the buckling response of laminated composite plates are obtained and efficiency of the method is considered. Numerical results with different element order are presented and the obtained results are compared to analytical and conventional numerical results as well as existing isogeometric plate finite elements.</description><subject>Buckling</subject><subject>Composite structures</subject><subject>Computational efficiency</subject><subject>Finite element method</subject><subject>Free vibration</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Plates (structural members)</subject><issn>1429-2955</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNotkD1vgzAURRlaqVGaH9DNYxeoP7CBkRAHrBKMgFTqZJkvKRFpKE6G_vuSpst9uk_nveFY1guCDqKM4LfjRZ_scXAocbDjUvJgLZCLAxsHlD5ZK2OOEELsUxYQuLDO24Jz8CHWRVgJmYEw24D1PnpPRRbPJUw_S1ECuQWJiBNeAFls5kzDncjCim9AJHe5LEXFQZ7OixLsy9tllXAgShlzueNVISIQ5nkhwyh5th57PZhu9T-X1n7LqyixUxmLKEztBnv-xa7dFndeTSnr28b1fMg0azTEWLd-XzOECWaI6aaHQR0EENa0RYgh4rO6a4Iak6X1ev87Tufva2cu6nQwTTcM-qs7X41CHsPQC5jLZhTd0WY6GzN1vRqnw0lPPwpB9edU3ZyqcVCUKKxmp-QXkhhkIA</recordid><startdate>20150101</startdate><enddate>20150101</enddate><creator>Peković, Ognjen</creator><creator>Stupar, Slobodan</creator><creator>Simonović, Aleksandar</creator><creator>Svorcan, Jelena</creator><creator>Trivković, Srdan</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>20150101</creationdate><title>FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH</title><author>Peković, Ognjen ; Stupar, Slobodan ; Simonović, Aleksandar ; Svorcan, Jelena ; Trivković, Srdan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c278t-b4d2e7b556fdc47806a6ca022ad8fb61232616acf09b9900b5d1161386bec9b23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Buckling</topic><topic>Composite structures</topic><topic>Computational efficiency</topic><topic>Finite element method</topic><topic>Free vibration</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Plates (structural members)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Peković, Ognjen</creatorcontrib><creatorcontrib>Stupar, Slobodan</creatorcontrib><creatorcontrib>Simonović, Aleksandar</creatorcontrib><creatorcontrib>Svorcan, Jelena</creatorcontrib><creatorcontrib>Trivković, Srdan</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of Theoretical and Applied Mechanics (Warsaw)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Peković, Ognjen</au><au>Stupar, Slobodan</au><au>Simonović, Aleksandar</au><au>Svorcan, Jelena</au><au>Trivković, Srdan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH</atitle><jtitle>Journal of Theoretical and Applied Mechanics (Warsaw)</jtitle><date>2015-01-01</date><risdate>2015</risdate><volume>53</volume><issue>2</issue><spage>453</spage><epage>466</epage><pages>453-466</pages><issn>1429-2955</issn><abstract>This research paper presents a higher order isogeometric laminated composite plate finite element formulation. The isogeometric formulation is based on NURBS (non-uniform rational B-splines) basis functions of varying degree. Plate kinematics is based on the third order shear deformation theory (TSDT) of Reddy in order to avoid shear locking. Free vibration and the buckling response of laminated composite plates are obtained and efficiency of the method is considered. Numerical results with different element order are presented and the obtained results are compared to analytical and conventional numerical results as well as existing isogeometric plate finite elements.</abstract><doi>10.15632/jtam-pl.53.2.453</doi><tpages>14</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1429-2955
ispartof Journal of Theoretical and Applied Mechanics (Warsaw), 2015-01, Vol.53 (2), p.453-466
issn 1429-2955
language eng
recordid cdi_proquest_miscellaneous_1762079646
source Alma/SFX Local Collection
subjects Buckling
Composite structures
Computational efficiency
Finite element method
Free vibration
Mathematical analysis
Mathematical models
Plates (structural members)
title FREE VIBRATION AND BUCKLING ANALYSIS OF HIGHER ORDER LAMINATED COMPOSITE PLATES USING THE ISOGEOMETRIC APPROACH
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-12T15%3A55%3A58IST&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=FREE%20VIBRATION%20AND%20BUCKLING%20ANALYSIS%20OF%20HIGHER%20ORDER%20LAMINATED%20COMPOSITE%20PLATES%20USING%20THE%20ISOGEOMETRIC%20APPROACH&rft.jtitle=Journal%20of%20Theoretical%20and%20Applied%20Mechanics%20(Warsaw)&rft.au=Pekovi%C4%87,%20Ognjen&rft.date=2015-01-01&rft.volume=53&rft.issue=2&rft.spage=453&rft.epage=466&rft.pages=453-466&rft.issn=1429-2955&rft_id=info:doi/10.15632/jtam-pl.53.2.453&rft_dat=%3Cproquest_cross%3E1762079646%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=1762079646&rft_id=info:pmid/&rfr_iscdi=true