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An efficient 3-node triangular plate element for static and dynamic analyses of microplates based on modified couple stress theory with micro-inertia
Within the modified couple stress elasticity, a novel nonconforming 3-node triangular plate element is derived from the d’Alembert–Lagrange principle for simulating the size-dependent static and dynamic bending behaviors of thin microplates and studying the effects of micro-inertia. This is accompli...
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Published in: | Engineering with computers 2023-10, Vol.39 (5), p.3061-3084 |
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creator | Mao, Yu-Hao Shang, Yan Cen, Song Li, Chen-Feng |
description | Within the modified couple stress elasticity, a novel nonconforming 3-node triangular plate element is derived from the d’Alembert–Lagrange principle for simulating the size-dependent static and dynamic bending behaviors of thin microplates and studying the effects of micro-inertia. This is accomplished via two main steps. First, the Trefftz functions that are derived from the governing equations of the problem concerned are adopted as the basis functions for constructing the element’s displacement interpolation. Second, according to the generalized conforming theory, the SemiLoof constraints are used to enforce the
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1
compatibility requirement for guaranteeing the computation convergence. The benchmark tests are carried out and the results reveal that the new element exhibits satisfactory numerical accuracy and captures the size dependences effectively in the static, free vibration and forced vibration analyses. Moreover, the findings also show that the micro-inertia affects the dynamic response of the plate mainly through the natural frequency. In general, the influences on higher order modes are more obvious than that on lower order modes. |
doi_str_mv | 10.1007/s00366-022-01715-5 |
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C
1
compatibility requirement for guaranteeing the computation convergence. The benchmark tests are carried out and the results reveal that the new element exhibits satisfactory numerical accuracy and captures the size dependences effectively in the static, free vibration and forced vibration analyses. Moreover, the findings also show that the micro-inertia affects the dynamic response of the plate mainly through the natural frequency. In general, the influences on higher order modes are more obvious than that on lower order modes.</description><identifier>ISSN: 0177-0667</identifier><identifier>EISSN: 1435-5663</identifier><identifier>DOI: 10.1007/s00366-022-01715-5</identifier><language>eng</language><publisher>London: Springer London</publisher><subject>Aerospace engineering ; Basis functions ; CAE) and Design ; Calculus of Variations and Optimal Control; Optimization ; Classical Mechanics ; Computer Science ; Computer-Aided Engineering (CAD ; Control ; Dynamic response ; Forced vibration ; Free vibration ; Inertia ; Interpolation ; Math. Applications in Chemistry ; Mathematical and Computational Engineering ; Mechanics ; Original Article ; Resonant frequencies ; Systems Theory</subject><ispartof>Engineering with computers, 2023-10, Vol.39 (5), p.3061-3084</ispartof><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2022</rights><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-fa6d9f0262ba57ccee8842f9d389656c014aa85869ff9bf4729041c6805862fc3</citedby><cites>FETCH-LOGICAL-c319t-fa6d9f0262ba57ccee8842f9d389656c014aa85869ff9bf4729041c6805862fc3</cites><orcidid>0000-0001-9869-5039</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Mao, Yu-Hao</creatorcontrib><creatorcontrib>Shang, Yan</creatorcontrib><creatorcontrib>Cen, Song</creatorcontrib><creatorcontrib>Li, Chen-Feng</creatorcontrib><title>An efficient 3-node triangular plate element for static and dynamic analyses of microplates based on modified couple stress theory with micro-inertia</title><title>Engineering with computers</title><addtitle>Engineering with Computers</addtitle><description>Within the modified couple stress elasticity, a novel nonconforming 3-node triangular plate element is derived from the d’Alembert–Lagrange principle for simulating the size-dependent static and dynamic bending behaviors of thin microplates and studying the effects of micro-inertia. This is accomplished via two main steps. First, the Trefftz functions that are derived from the governing equations of the problem concerned are adopted as the basis functions for constructing the element’s displacement interpolation. Second, according to the generalized conforming theory, the SemiLoof constraints are used to enforce the
C
1
compatibility requirement for guaranteeing the computation convergence. The benchmark tests are carried out and the results reveal that the new element exhibits satisfactory numerical accuracy and captures the size dependences effectively in the static, free vibration and forced vibration analyses. Moreover, the findings also show that the micro-inertia affects the dynamic response of the plate mainly through the natural frequency. In general, the influences on higher order modes are more obvious than that on lower order modes.</description><subject>Aerospace engineering</subject><subject>Basis functions</subject><subject>CAE) and Design</subject><subject>Calculus of Variations and Optimal Control; Optimization</subject><subject>Classical Mechanics</subject><subject>Computer Science</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Control</subject><subject>Dynamic response</subject><subject>Forced vibration</subject><subject>Free vibration</subject><subject>Inertia</subject><subject>Interpolation</subject><subject>Math. Applications in Chemistry</subject><subject>Mathematical and Computational Engineering</subject><subject>Mechanics</subject><subject>Original Article</subject><subject>Resonant frequencies</subject><subject>Systems Theory</subject><issn>0177-0667</issn><issn>1435-5663</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNp9kM1uGyEUhVGUSnHcvEBWSF3TXGCGGZaW1T8pUjfJGmHmkmCNwQWsyg_S9y3xVMquKw6X8x1dDiH3HD5zgOGhAEilGAjBgA-8Z_0VWfFONqGUvCarNh0YKDXckNtS9gBcAugV-bOJFL0PLmCsVLKYJqQ1BxtfTrPN9DjbihRnPLy9-5RpqbYGR22c6HSO9nDRdj4XLDR52u45XahCd7bgRFOkhzQFH5p26XScsWVkLIXWV0z5TH-H-rpwLETMNdiP5IO3c8G7f-eaPH_98rT9zh5_fvux3TwyJ7muzFs1aQ9CiZ3tB-cQx7ETXk9y1KpXDnhn7diPSnuvd74bhIaOOzVCmwnv5Jp8WnKPOf06Yalmn065_aYYMaqxG7SSsrnE4moblpLRm2MOB5vPhoN5q98s9ZtWv7nUb_oGyQUqzRxfML9H_4f6C_5qip8</recordid><startdate>20231001</startdate><enddate>20231001</enddate><creator>Mao, Yu-Hao</creator><creator>Shang, Yan</creator><creator>Cen, Song</creator><creator>Li, Chen-Feng</creator><general>Springer London</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>3V.</scope><scope>7SC</scope><scope>7TB</scope><scope>7XB</scope><scope>8AL</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>JQ2</scope><scope>K7-</scope><scope>KR7</scope><scope>L6V</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>M0N</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>Q9U</scope><orcidid>https://orcid.org/0000-0001-9869-5039</orcidid></search><sort><creationdate>20231001</creationdate><title>An efficient 3-node triangular plate element for static and dynamic analyses of microplates based on modified couple stress theory with micro-inertia</title><author>Mao, Yu-Hao ; Shang, Yan ; Cen, Song ; Li, Chen-Feng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-fa6d9f0262ba57ccee8842f9d389656c014aa85869ff9bf4729041c6805862fc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aerospace engineering</topic><topic>Basis functions</topic><topic>CAE) and Design</topic><topic>Calculus of Variations and Optimal Control; Optimization</topic><topic>Classical Mechanics</topic><topic>Computer Science</topic><topic>Computer-Aided Engineering (CAD</topic><topic>Control</topic><topic>Dynamic response</topic><topic>Forced vibration</topic><topic>Free vibration</topic><topic>Inertia</topic><topic>Interpolation</topic><topic>Math. Applications in Chemistry</topic><topic>Mathematical and Computational Engineering</topic><topic>Mechanics</topic><topic>Original Article</topic><topic>Resonant frequencies</topic><topic>Systems Theory</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Mao, Yu-Hao</creatorcontrib><creatorcontrib>Shang, Yan</creatorcontrib><creatorcontrib>Cen, Song</creatorcontrib><creatorcontrib>Li, Chen-Feng</creatorcontrib><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>Computer and Information Systems Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Computing Database (Alumni Edition)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Engineering Research Database</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Computer Science Collection</collection><collection>Computer Science Database</collection><collection>Civil Engineering Abstracts</collection><collection>ProQuest Engineering Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>Computing Database</collection><collection>Engineering Database</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>Engineering Collection</collection><collection>ProQuest Central Basic</collection><jtitle>Engineering with computers</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mao, Yu-Hao</au><au>Shang, Yan</au><au>Cen, Song</au><au>Li, Chen-Feng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>An efficient 3-node triangular plate element for static and dynamic analyses of microplates based on modified couple stress theory with micro-inertia</atitle><jtitle>Engineering with computers</jtitle><stitle>Engineering with Computers</stitle><date>2023-10-01</date><risdate>2023</risdate><volume>39</volume><issue>5</issue><spage>3061</spage><epage>3084</epage><pages>3061-3084</pages><issn>0177-0667</issn><eissn>1435-5663</eissn><abstract>Within the modified couple stress elasticity, a novel nonconforming 3-node triangular plate element is derived from the d’Alembert–Lagrange principle for simulating the size-dependent static and dynamic bending behaviors of thin microplates and studying the effects of micro-inertia. This is accomplished via two main steps. First, the Trefftz functions that are derived from the governing equations of the problem concerned are adopted as the basis functions for constructing the element’s displacement interpolation. Second, according to the generalized conforming theory, the SemiLoof constraints are used to enforce the
C
1
compatibility requirement for guaranteeing the computation convergence. The benchmark tests are carried out and the results reveal that the new element exhibits satisfactory numerical accuracy and captures the size dependences effectively in the static, free vibration and forced vibration analyses. Moreover, the findings also show that the micro-inertia affects the dynamic response of the plate mainly through the natural frequency. In general, the influences on higher order modes are more obvious than that on lower order modes.</abstract><cop>London</cop><pub>Springer London</pub><doi>10.1007/s00366-022-01715-5</doi><tpages>24</tpages><orcidid>https://orcid.org/0000-0001-9869-5039</orcidid></addata></record> |
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subjects | Aerospace engineering Basis functions CAE) and Design Calculus of Variations and Optimal Control Optimization Classical Mechanics Computer Science Computer-Aided Engineering (CAD Control Dynamic response Forced vibration Free vibration Inertia Interpolation Math. Applications in Chemistry Mathematical and Computational Engineering Mechanics Original Article Resonant frequencies Systems Theory |
title | An efficient 3-node triangular plate element for static and dynamic analyses of microplates based on modified couple stress theory with micro-inertia |
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