Eigen-frequency analysis of spherical shell laminated composite plates with and without central cutouts using finite elements
This article presents the free vibration responses of spherical shell laminated composite panels (SSLCP) without and with central cutouts (square, circular and rectangular) using finite elements. The SSLCP midplane kinematics has been modeled using ABAQUS commercial finite element tool in the framew...
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Veröffentlicht in: | IOP conference series. Materials Science and Engineering 2018-07, Vol.390 (1), p.12043 |
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description | This article presents the free vibration responses of spherical shell laminated composite panels (SSLCP) without and with central cutouts (square, circular and rectangular) using finite elements. The SSLCP midplane kinematics has been modeled using ABAQUS commercial finite element tool in the framework of first order shear deformation theory. Firstly, the validity of the present model is established by comparing the present natural frequencies values with the available benchmark results. Subsequently, the influence of both varying and constant aspect ratio for different central cutouts on the natural frequencies of SSLCP are investigated by solving appropriate numerical examples and findings are discussed in detail. The results are given in the form of tables and figures. |
doi_str_mv | 10.1088/1757-899X/390/1/012043 |
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The SSLCP midplane kinematics has been modeled using ABAQUS commercial finite element tool in the framework of first order shear deformation theory. Firstly, the validity of the present model is established by comparing the present natural frequencies values with the available benchmark results. Subsequently, the influence of both varying and constant aspect ratio for different central cutouts on the natural frequencies of SSLCP are investigated by solving appropriate numerical examples and findings are discussed in detail. 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The results are given in the form of tables and figures.</description><subject>Aspect ratio</subject><subject>Composite structures</subject><subject>Finite element method</subject><subject>Free vibration</subject><subject>Frequency analysis</subject><subject>Kinematics</subject><subject>Laminar composites</subject><subject>Mathematical models</subject><subject>Resonant frequencies</subject><subject>Shear deformation</subject><subject>Spherical shells</subject><subject>Vibration response</subject><issn>1757-8981</issn><issn>1757-899X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNqFkEtLxDAUhYMoOI7-BQm4cVN706SPLGUYHzDiQgV3IU3TmQx9mbTILPzvplZGBMHVfZ3vwD0InRO4IpBlIUnjNMg4fw0ph5CEQCJg9ADN9ofDfZ-RY3Ti3BYgSRmDGfpYmrVugtLqt0E3aodlI6udMw63JXbdRlujZIXdRlcVrmRtGtnrAqu27lpneo27yi8cfjf9xrPFV9MOPVa66a0n1dD70eHBmWaNS9OMkK507e_uFB2VsnL67LvO0cvN8nlxF6web-8X16tAMUj7gPNcqRwoySgpGYkzQrRUCc1zyuIUIGPAYiA0JlwmrCgjyEmitOIqSjJQOZ2ji8m3s63_0_Vi2w7Wf-pEFHsHxhnjXpVMKmVb56wuRWdNLe1OEBBj1GJMUYyJCh-1IGKK2oPRBJq2-3H-F7r8A3p4Wv6Sia4o6SeTApAE</recordid><startdate>20180701</startdate><enddate>20180701</enddate><creator>Behera, Ranjan K.</creator><creator>Garg, Kushagra</creator><creator>Patro, Sudhansu S.</creator><creator>Sharma, Nitin</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20180701</creationdate><title>Eigen-frequency analysis of spherical shell laminated composite plates with and without central cutouts using finite elements</title><author>Behera, Ranjan K. ; Garg, Kushagra ; Patro, Sudhansu S. ; Sharma, Nitin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c407t-99bccb031831f415811eac63bb34570084045013519a64df20b16cec9c2680cb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aspect ratio</topic><topic>Composite structures</topic><topic>Finite element method</topic><topic>Free vibration</topic><topic>Frequency analysis</topic><topic>Kinematics</topic><topic>Laminar composites</topic><topic>Mathematical models</topic><topic>Resonant frequencies</topic><topic>Shear deformation</topic><topic>Spherical shells</topic><topic>Vibration response</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Behera, Ranjan K.</creatorcontrib><creatorcontrib>Garg, Kushagra</creatorcontrib><creatorcontrib>Patro, Sudhansu S.</creatorcontrib><creatorcontrib>Sharma, Nitin</creatorcontrib><collection>IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection (ProQuest)</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Science Database</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Materials Science Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>IOP conference series. 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The SSLCP midplane kinematics has been modeled using ABAQUS commercial finite element tool in the framework of first order shear deformation theory. Firstly, the validity of the present model is established by comparing the present natural frequencies values with the available benchmark results. Subsequently, the influence of both varying and constant aspect ratio for different central cutouts on the natural frequencies of SSLCP are investigated by solving appropriate numerical examples and findings are discussed in detail. The results are given in the form of tables and figures.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1757-899X/390/1/012043</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aspect ratio Composite structures Finite element method Free vibration Frequency analysis Kinematics Laminar composites Mathematical models Resonant frequencies Shear deformation Spherical shells Vibration response |
title | Eigen-frequency analysis of spherical shell laminated composite plates with and without central cutouts using finite elements |
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