Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory
Two new C 0 assumed strain finite element formulations of Reddy's higher-order theory are used to determine the natural frequencies of isotropic, orthotropic, and layered anisotropic composite and sandwich plates. The material properties typical of glass fibre polyester resins for the skin and...
Gespeichert in:
| Veröffentlicht in: | Composites. Part B, Engineering Engineering, 2002-01, Vol.33 (7), p.505-519 |
|---|---|
| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 519 |
|---|---|
| container_issue | 7 |
| container_start_page | 505 |
| container_title | Composites. Part B, Engineering |
| container_volume | 33 |
| creator | Nayak, A.K. Moy, S.S.J. Shenoi, R.A. |
| description | Two new
C
0 assumed strain finite element formulations of Reddy's higher-order theory are used to determine the natural frequencies of isotropic, orthotropic, and layered anisotropic composite and sandwich plates. The material properties typical of glass fibre polyester resins for the skin and HEREX C70 PVC (polyvinyl chloride) foam materials for the core are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, degree of orthotropy, number of layers and lamination scheme on the natural frequencies. A consistent mass matrix is adopted in the present formulation. The results presented in this investigation could be useful for a better understanding of the behaviour of sandwich laminates under free vibration conditions and potentially beneficial for designers of sandwich structures. |
| doi_str_mv | 10.1016/S1359-8368(02)00035-5 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_27154598</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S1359836802000355</els_id><sourcerecordid>27154598</sourcerecordid><originalsourceid>FETCH-LOGICAL-c368t-9d07560e445c81742b78ad676d1268b1e9d0e23e232d0248f37183ee13e4274d3</originalsourceid><addsrcrecordid>eNqFkElLBDEQhRtRcP0JQi5uh9as3emTyOAGguBy8BQySbUT6emMqXZk_r3RGfEoFFQdvlev6hXFPqOnjLLq7JEJ1ZRaVPqY8hNKqVClWiu2mK6bktGqWc_zL7JZbCO-ZUgqwbeKl6sEQOZhnOwQYk9sb7sFBiSxJS5OZxHDAARt7z-Dm5BZZwdAMrYInmT8AbxfHCGZhNcJpDImD4kME4hpsVtstLZD2Fv1neL56vJpdFPe3V_fji7uSpevGcrG01pVFKRUTrNa8nGtra_qyjNe6TGDDAAXubinXOpW1EwLACZA8lp6sVMcLvfOUnz_ABzMNKCDrrM9xA80vGZKqkZnUC1BlyJigtbMUpjatDCMmu8gzU-Q5jslQ7n5CdKorDtYGVh0tmuT7V3AP7FoZMManrnzJQf523mAZNAF6B34kMANxsfwj9MXJLCHBQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27154598</pqid></control><display><type>article</type><title>Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory</title><source>ScienceDirect Journals (5 years ago - present)</source><creator>Nayak, A.K. ; Moy, S.S.J. ; Shenoi, R.A.</creator><creatorcontrib>Nayak, A.K. ; Moy, S.S.J. ; Shenoi, R.A.</creatorcontrib><description>Two new
C
0 assumed strain finite element formulations of Reddy's higher-order theory are used to determine the natural frequencies of isotropic, orthotropic, and layered anisotropic composite and sandwich plates. The material properties typical of glass fibre polyester resins for the skin and HEREX C70 PVC (polyvinyl chloride) foam materials for the core are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, degree of orthotropy, number of layers and lamination scheme on the natural frequencies. A consistent mass matrix is adopted in the present formulation. The results presented in this investigation could be useful for a better understanding of the behaviour of sandwich laminates under free vibration conditions and potentially beneficial for designers of sandwich structures.</description><identifier>ISSN: 1359-8368</identifier><identifier>EISSN: 1879-1069</identifier><identifier>DOI: 10.1016/S1359-8368(02)00035-5</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Applied sciences ; Exact sciences and technology ; Forms of application and semi-finished materials ; Free vibration ; Laminates ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Composites. Part B, Engineering, 2002-01, Vol.33 (7), p.505-519</ispartof><rights>2002 Elsevier Science Ltd</rights><rights>2003 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c368t-9d07560e445c81742b78ad676d1268b1e9d0e23e232d0248f37183ee13e4274d3</citedby><cites>FETCH-LOGICAL-c368t-9d07560e445c81742b78ad676d1268b1e9d0e23e232d0248f37183ee13e4274d3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/S1359-8368(02)00035-5$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3548,27923,27924,45994</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=13949192$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Nayak, A.K.</creatorcontrib><creatorcontrib>Moy, S.S.J.</creatorcontrib><creatorcontrib>Shenoi, R.A.</creatorcontrib><title>Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory</title><title>Composites. Part B, Engineering</title><description>Two new
C
0 assumed strain finite element formulations of Reddy's higher-order theory are used to determine the natural frequencies of isotropic, orthotropic, and layered anisotropic composite and sandwich plates. The material properties typical of glass fibre polyester resins for the skin and HEREX C70 PVC (polyvinyl chloride) foam materials for the core are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, degree of orthotropy, number of layers and lamination scheme on the natural frequencies. A consistent mass matrix is adopted in the present formulation. The results presented in this investigation could be useful for a better understanding of the behaviour of sandwich laminates under free vibration conditions and potentially beneficial for designers of sandwich structures.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Free vibration</subject><subject>Laminates</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>1359-8368</issn><issn>1879-1069</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><recordid>eNqFkElLBDEQhRtRcP0JQi5uh9as3emTyOAGguBy8BQySbUT6emMqXZk_r3RGfEoFFQdvlev6hXFPqOnjLLq7JEJ1ZRaVPqY8hNKqVClWiu2mK6bktGqWc_zL7JZbCO-ZUgqwbeKl6sEQOZhnOwQYk9sb7sFBiSxJS5OZxHDAARt7z-Dm5BZZwdAMrYInmT8AbxfHCGZhNcJpDImD4kME4hpsVtstLZD2Fv1neL56vJpdFPe3V_fji7uSpevGcrG01pVFKRUTrNa8nGtra_qyjNe6TGDDAAXubinXOpW1EwLACZA8lp6sVMcLvfOUnz_ABzMNKCDrrM9xA80vGZKqkZnUC1BlyJigtbMUpjatDCMmu8gzU-Q5jslQ7n5CdKorDtYGVh0tmuT7V3AP7FoZMManrnzJQf523mAZNAF6B34kMANxsfwj9MXJLCHBQ</recordid><startdate>20020101</startdate><enddate>20020101</enddate><creator>Nayak, A.K.</creator><creator>Moy, S.S.J.</creator><creator>Shenoi, R.A.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><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>20020101</creationdate><title>Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory</title><author>Nayak, A.K. ; Moy, S.S.J. ; Shenoi, R.A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-9d07560e445c81742b78ad676d1268b1e9d0e23e232d0248f37183ee13e4274d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Free vibration</topic><topic>Laminates</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Nayak, A.K.</creatorcontrib><creatorcontrib>Moy, S.S.J.</creatorcontrib><creatorcontrib>Shenoi, R.A.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & 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>Composites. Part B, Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Nayak, A.K.</au><au>Moy, S.S.J.</au><au>Shenoi, R.A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory</atitle><jtitle>Composites. Part B, Engineering</jtitle><date>2002-01-01</date><risdate>2002</risdate><volume>33</volume><issue>7</issue><spage>505</spage><epage>519</epage><pages>505-519</pages><issn>1359-8368</issn><eissn>1879-1069</eissn><abstract>Two new
C
0 assumed strain finite element formulations of Reddy's higher-order theory are used to determine the natural frequencies of isotropic, orthotropic, and layered anisotropic composite and sandwich plates. The material properties typical of glass fibre polyester resins for the skin and HEREX C70 PVC (polyvinyl chloride) foam materials for the core are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, degree of orthotropy, number of layers and lamination scheme on the natural frequencies. A consistent mass matrix is adopted in the present formulation. The results presented in this investigation could be useful for a better understanding of the behaviour of sandwich laminates under free vibration conditions and potentially beneficial for designers of sandwich structures.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/S1359-8368(02)00035-5</doi><tpages>15</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1359-8368 |
| ispartof | Composites. Part B, Engineering, 2002-01, Vol.33 (7), p.505-519 |
| issn | 1359-8368 1879-1069 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_27154598 |
| source | ScienceDirect Journals (5 years ago - present) |
| subjects | Applied sciences Exact sciences and technology Forms of application and semi-finished materials Free vibration Laminates Polymer industry, paints, wood Technology of polymers |
| title | Free vibration analysis of composite sandwich plates based on Reddy's higher-order theory |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-12T19%3A27%3A23IST&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%20analysis%20of%20composite%20sandwich%20plates%20based%20on%20Reddy's%20higher-order%20theory&rft.jtitle=Composites.%20Part%20B,%20Engineering&rft.au=Nayak,%20A.K.&rft.date=2002-01-01&rft.volume=33&rft.issue=7&rft.spage=505&rft.epage=519&rft.pages=505-519&rft.issn=1359-8368&rft.eissn=1879-1069&rft_id=info:doi/10.1016/S1359-8368(02)00035-5&rft_dat=%3Cproquest_cross%3E27154598%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=27154598&rft_id=info:pmid/&rft_els_id=S1359836802000355&rfr_iscdi=true |