Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel
The present study deals with buckling analysis of simply supported conical panels based on the Donnell's shell theory. Different material properties have been considered such as isotropic, composite laminated and functionally graded (FG). The governing differential equation for buckling of lami...
Gespeichert in:
| Veröffentlicht in: | Composites. Part B, Engineering Engineering, 2016-06, Vol.94, p.1-10 |
|---|---|
| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 10 |
|---|---|
| container_issue | |
| container_start_page | 1 |
| container_title | Composites. Part B, Engineering |
| container_volume | 94 |
| creator | Demir, Çiğdem Mercan, Kadir Civalek, Ömer |
| description | The present study deals with buckling analysis of simply supported conical panels based on the Donnell's shell theory. Different material properties have been considered such as isotropic, composite laminated and functionally graded (FG). The governing differential equation for buckling of laminated conical panel is derived. These equations are discrete using method of discrete singular convolution (DSC). Shannon's delta kernel is used for trial functions. To check the presented DSC method and computer program, the critical buckling loads for isotropic and composite conical panels are calculated which compare very well with earlier available results. The effect of some geometric parameters and material parameters on critical buckling of panels is also investigated. It is noticed that the present DSC methodology can predict accurately the buckling loads of conical panels. |
| doi_str_mv | 10.1016/j.compositesb.2016.03.031 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1816044606</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S1359836816300555</els_id><sourcerecordid>1816044606</sourcerecordid><originalsourceid>FETCH-LOGICAL-c354t-54eb9033d54ba4eaea4371107fc0f74c451acedbe81a27ca342aa2e7048a79693</originalsourceid><addsrcrecordid>eNqNUMtOwzAQjBBIlMI_mBsHEuzYeR1RoQWpiAuczcbZIJfEDraLxN_jthw4Iq20o92Z0e4kySWjGaOsvNlkyo6T9Tqgb7M8jjLKY7GjZMbqqkkZLZvjiHnRpDUv69PkzPsNpVQUPJ8lb3cY0I3aQNDWENsT5XTQCgbSbtXHoM07GSx0frfS3gZnJ62uyXL1RMB0ZIC9FjsS3NaoPVLW7A0mMDicJyc9DB4vfvs8eV3evywe0vXz6nFxu04VL0RIC4FtQznvCtGCQEAQvGKMVr2ifSWUKBgo7FqsGeSVAi5ygBwrKmqomrLh8-Tq4Ds5-7lFH-SovcJhiEfYrZesZiUVoqRlpDYHqnLWe4e9nJwewX1LRuUuVbmRf1KVu1Ql5bFY1C4OWoy_fGl00iuNJp6mHaogO6v_4fIDE1mINg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1816044606</pqid></control><display><type>article</type><title>Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel</title><source>Access via ScienceDirect (Elsevier)</source><creator>Demir, Çiğdem ; Mercan, Kadir ; Civalek, Ömer</creator><creatorcontrib>Demir, Çiğdem ; Mercan, Kadir ; Civalek, Ömer</creatorcontrib><description>The present study deals with buckling analysis of simply supported conical panels based on the Donnell's shell theory. Different material properties have been considered such as isotropic, composite laminated and functionally graded (FG). The governing differential equation for buckling of laminated conical panel is derived. These equations are discrete using method of discrete singular convolution (DSC). Shannon's delta kernel is used for trial functions. To check the presented DSC method and computer program, the critical buckling loads for isotropic and composite conical panels are calculated which compare very well with earlier available results. The effect of some geometric parameters and material parameters on critical buckling of panels is also investigated. It is noticed that the present DSC methodology can predict accurately the buckling loads of conical panels.</description><identifier>ISSN: 1359-8368</identifier><identifier>EISSN: 1879-1069</identifier><identifier>DOI: 10.1016/j.compositesb.2016.03.031</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>A. Lamina/ply ; B. Buckling ; Buckling ; C. Computational modelling ; Computer programs ; Deltas ; Differential equations ; Functionally gradient materials ; Kernels ; Mathematical analysis ; Panels</subject><ispartof>Composites. Part B, Engineering, 2016-06, Vol.94, p.1-10</ispartof><rights>2016 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c354t-54eb9033d54ba4eaea4371107fc0f74c451acedbe81a27ca342aa2e7048a79693</citedby><cites>FETCH-LOGICAL-c354t-54eb9033d54ba4eaea4371107fc0f74c451acedbe81a27ca342aa2e7048a79693</cites><orcidid>0000-0003-1907-9479</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.compositesb.2016.03.031$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3550,27924,27925,45995</link.rule.ids></links><search><creatorcontrib>Demir, Çiğdem</creatorcontrib><creatorcontrib>Mercan, Kadir</creatorcontrib><creatorcontrib>Civalek, Ömer</creatorcontrib><title>Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel</title><title>Composites. Part B, Engineering</title><description>The present study deals with buckling analysis of simply supported conical panels based on the Donnell's shell theory. Different material properties have been considered such as isotropic, composite laminated and functionally graded (FG). The governing differential equation for buckling of laminated conical panel is derived. These equations are discrete using method of discrete singular convolution (DSC). Shannon's delta kernel is used for trial functions. To check the presented DSC method and computer program, the critical buckling loads for isotropic and composite conical panels are calculated which compare very well with earlier available results. The effect of some geometric parameters and material parameters on critical buckling of panels is also investigated. It is noticed that the present DSC methodology can predict accurately the buckling loads of conical panels.</description><subject>A. Lamina/ply</subject><subject>B. Buckling</subject><subject>Buckling</subject><subject>C. Computational modelling</subject><subject>Computer programs</subject><subject>Deltas</subject><subject>Differential equations</subject><subject>Functionally gradient materials</subject><subject>Kernels</subject><subject>Mathematical analysis</subject><subject>Panels</subject><issn>1359-8368</issn><issn>1879-1069</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNqNUMtOwzAQjBBIlMI_mBsHEuzYeR1RoQWpiAuczcbZIJfEDraLxN_jthw4Iq20o92Z0e4kySWjGaOsvNlkyo6T9Tqgb7M8jjLKY7GjZMbqqkkZLZvjiHnRpDUv69PkzPsNpVQUPJ8lb3cY0I3aQNDWENsT5XTQCgbSbtXHoM07GSx0frfS3gZnJ62uyXL1RMB0ZIC9FjsS3NaoPVLW7A0mMDicJyc9DB4vfvs8eV3evywe0vXz6nFxu04VL0RIC4FtQznvCtGCQEAQvGKMVr2ifSWUKBgo7FqsGeSVAi5ygBwrKmqomrLh8-Tq4Ds5-7lFH-SovcJhiEfYrZesZiUVoqRlpDYHqnLWe4e9nJwewX1LRuUuVbmRf1KVu1Ql5bFY1C4OWoy_fGl00iuNJp6mHaogO6v_4fIDE1mINg</recordid><startdate>20160601</startdate><enddate>20160601</enddate><creator>Demir, Çiğdem</creator><creator>Mercan, Kadir</creator><creator>Civalek, Ömer</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope><orcidid>https://orcid.org/0000-0003-1907-9479</orcidid></search><sort><creationdate>20160601</creationdate><title>Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel</title><author>Demir, Çiğdem ; Mercan, Kadir ; Civalek, Ömer</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c354t-54eb9033d54ba4eaea4371107fc0f74c451acedbe81a27ca342aa2e7048a79693</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>A. Lamina/ply</topic><topic>B. Buckling</topic><topic>Buckling</topic><topic>C. Computational modelling</topic><topic>Computer programs</topic><topic>Deltas</topic><topic>Differential equations</topic><topic>Functionally gradient materials</topic><topic>Kernels</topic><topic>Mathematical analysis</topic><topic>Panels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Demir, Çiğdem</creatorcontrib><creatorcontrib>Mercan, Kadir</creatorcontrib><creatorcontrib>Civalek, Ömer</creatorcontrib><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>Demir, Çiğdem</au><au>Mercan, Kadir</au><au>Civalek, Ömer</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel</atitle><jtitle>Composites. Part B, Engineering</jtitle><date>2016-06-01</date><risdate>2016</risdate><volume>94</volume><spage>1</spage><epage>10</epage><pages>1-10</pages><issn>1359-8368</issn><eissn>1879-1069</eissn><abstract>The present study deals with buckling analysis of simply supported conical panels based on the Donnell's shell theory. Different material properties have been considered such as isotropic, composite laminated and functionally graded (FG). The governing differential equation for buckling of laminated conical panel is derived. These equations are discrete using method of discrete singular convolution (DSC). Shannon's delta kernel is used for trial functions. To check the presented DSC method and computer program, the critical buckling loads for isotropic and composite conical panels are calculated which compare very well with earlier available results. The effect of some geometric parameters and material parameters on critical buckling of panels is also investigated. It is noticed that the present DSC methodology can predict accurately the buckling loads of conical panels.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.compositesb.2016.03.031</doi><tpages>10</tpages><orcidid>https://orcid.org/0000-0003-1907-9479</orcidid></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1359-8368 |
| ispartof | Composites. Part B, Engineering, 2016-06, Vol.94, p.1-10 |
| issn | 1359-8368 1879-1069 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_1816044606 |
| source | Access via ScienceDirect (Elsevier) |
| subjects | A. Lamina/ply B. Buckling Buckling C. Computational modelling Computer programs Deltas Differential equations Functionally gradient materials Kernels Mathematical analysis Panels |
| title | Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-19T06%3A08%3A11IST&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=Determination%20of%20critical%20buckling%20loads%20of%20isotropic,%20FGM%20and%20laminated%20truncated%20conical%20panel&rft.jtitle=Composites.%20Part%20B,%20Engineering&rft.au=Demir,%20%C3%87i%C4%9Fdem&rft.date=2016-06-01&rft.volume=94&rft.spage=1&rft.epage=10&rft.pages=1-10&rft.issn=1359-8368&rft.eissn=1879-1069&rft_id=info:doi/10.1016/j.compositesb.2016.03.031&rft_dat=%3Cproquest_cross%3E1816044606%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=1816044606&rft_id=info:pmid/&rft_els_id=S1359836816300555&rfr_iscdi=true |