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On the layerwise finite element formulation for static and free vibration analysis of functionally graded sandwich plates
This paper presents a novel C 0 higher-order layerwise finite element model for static and free vibration analysis of functionally graded materials (FGM) sandwich plates. The proposed layerwise model, which is developed for multilayer composite plates, supposes higher-order displacement field for th...
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Published in: | Engineering with computers 2022-12, Vol.38 (Suppl 5), p.3871-3899 |
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description | This paper presents a novel C
0
higher-order layerwise finite element model for static and free vibration analysis of functionally graded materials (FGM) sandwich plates. The proposed layerwise model, which is developed for multilayer composite plates, supposes higher-order displacement field for the core and first-order displacement field for the face sheets maintaining a continuity of displacement at layer. Unlike the conventional layerwise models, the present one has an important feature that the number of variables is fixed and does not increase when increasing the number of layers. Thus, based on the suggested model, a computationally efficient C
0
eight-node quadrilateral element is developed. Indeed, the new element is free of shear locking phenomenon without requiring any shear correction factors. Three common types of FGM plates, namely, (i) isotropic FGM plates; (ii) sandwich plates with FGM face sheets and homogeneous core and (iii) sandwich plates with homogeneous face sheets and FGM core, are considered in the present work. Material properties are assumed graded in the thickness direction according to a simple power law distribution in terms of the volume power laws of the constituents. The equations of motion of the FGM sandwich plate are obtained via the classical Hamilton’s principle. Numerical results of present model are compared with 2D, quasi-3D, and 3D analytical solutions and other predicted by advanced finite element models reported in the literature. The results indicate that the developed finite element model is promising in terms of accuracy and fast rate of convergence for both thin and thick FGM sandwich plates. Finally, it can be concluded that the proposed model is accurate and efficient in predicting the bending and free vibration responses of FGM sandwich plates. |
doi_str_mv | 10.1007/s00366-020-01250-1 |
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higher-order layerwise finite element model for static and free vibration analysis of functionally graded materials (FGM) sandwich plates. The proposed layerwise model, which is developed for multilayer composite plates, supposes higher-order displacement field for the core and first-order displacement field for the face sheets maintaining a continuity of displacement at layer. Unlike the conventional layerwise models, the present one has an important feature that the number of variables is fixed and does not increase when increasing the number of layers. Thus, based on the suggested model, a computationally efficient C
0
eight-node quadrilateral element is developed. Indeed, the new element is free of shear locking phenomenon without requiring any shear correction factors. Three common types of FGM plates, namely, (i) isotropic FGM plates; (ii) sandwich plates with FGM face sheets and homogeneous core and (iii) sandwich plates with homogeneous face sheets and FGM core, are considered in the present work. Material properties are assumed graded in the thickness direction according to a simple power law distribution in terms of the volume power laws of the constituents. The equations of motion of the FGM sandwich plate are obtained via the classical Hamilton’s principle. Numerical results of present model are compared with 2D, quasi-3D, and 3D analytical solutions and other predicted by advanced finite element models reported in the literature. The results indicate that the developed finite element model is promising in terms of accuracy and fast rate of convergence for both thin and thick FGM sandwich plates. Finally, it can be concluded that the proposed model is accurate and efficient in predicting the bending and free vibration responses of FGM sandwich plates.</description><identifier>ISSN: 0177-0667</identifier><identifier>EISSN: 1435-5663</identifier><identifier>DOI: 10.1007/s00366-020-01250-1</identifier><language>eng</language><publisher>London: Springer London</publisher><subject>CAE) and Design ; Calculus of Variations and Optimal Control; Optimization ; Classical Mechanics ; Composite structures ; Computer Science ; Computer-Aided Engineering (CAD ; Control ; Displacement ; Equations of motion ; Exact solutions ; Finite element method ; Free vibration ; Functionally gradient materials ; Hamilton's principle ; Material properties ; Math. Applications in Chemistry ; Mathematical and Computational Engineering ; Mathematical models ; Multilayers ; Original Article ; Plates (structural members) ; Quadrilaterals ; Sheets ; Systems Theory ; Two dimensional analysis ; Vibration analysis ; Vibration response</subject><ispartof>Engineering with computers, 2022-12, Vol.38 (Suppl 5), p.3871-3899</ispartof><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd. part of Springer Nature 2021</rights><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd. part of Springer Nature 2021.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-369d90fde7359a9e23109e9d0b5cd53fc375b2ad1ffc5ec8fb51f76bedf6d5943</citedby><cites>FETCH-LOGICAL-c319t-369d90fde7359a9e23109e9d0b5cd53fc375b2ad1ffc5ec8fb51f76bedf6d5943</cites><orcidid>0000-0002-5268-9925</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,778,782,27907,27908</link.rule.ids></links><search><creatorcontrib>Hirane, Hicham</creatorcontrib><creatorcontrib>Belarbi, Mohamed-Ouejdi</creatorcontrib><creatorcontrib>Houari, Mohammed Sid Ahmed</creatorcontrib><creatorcontrib>Tounsi, Abdelouahed</creatorcontrib><title>On the layerwise finite element formulation for static and free vibration analysis of functionally graded sandwich plates</title><title>Engineering with computers</title><addtitle>Engineering with Computers</addtitle><description>This paper presents a novel C
0
higher-order layerwise finite element model for static and free vibration analysis of functionally graded materials (FGM) sandwich plates. The proposed layerwise model, which is developed for multilayer composite plates, supposes higher-order displacement field for the core and first-order displacement field for the face sheets maintaining a continuity of displacement at layer. Unlike the conventional layerwise models, the present one has an important feature that the number of variables is fixed and does not increase when increasing the number of layers. Thus, based on the suggested model, a computationally efficient C
0
eight-node quadrilateral element is developed. Indeed, the new element is free of shear locking phenomenon without requiring any shear correction factors. Three common types of FGM plates, namely, (i) isotropic FGM plates; (ii) sandwich plates with FGM face sheets and homogeneous core and (iii) sandwich plates with homogeneous face sheets and FGM core, are considered in the present work. Material properties are assumed graded in the thickness direction according to a simple power law distribution in terms of the volume power laws of the constituents. The equations of motion of the FGM sandwich plate are obtained via the classical Hamilton’s principle. Numerical results of present model are compared with 2D, quasi-3D, and 3D analytical solutions and other predicted by advanced finite element models reported in the literature. The results indicate that the developed finite element model is promising in terms of accuracy and fast rate of convergence for both thin and thick FGM sandwich plates. Finally, it can be concluded that the proposed model is accurate and efficient in predicting the bending and free vibration responses of FGM sandwich plates.</description><subject>CAE) and Design</subject><subject>Calculus of Variations and Optimal Control; Optimization</subject><subject>Classical Mechanics</subject><subject>Composite structures</subject><subject>Computer Science</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Control</subject><subject>Displacement</subject><subject>Equations of motion</subject><subject>Exact solutions</subject><subject>Finite element method</subject><subject>Free vibration</subject><subject>Functionally gradient materials</subject><subject>Hamilton's principle</subject><subject>Material properties</subject><subject>Math. Applications in Chemistry</subject><subject>Mathematical and Computational Engineering</subject><subject>Mathematical models</subject><subject>Multilayers</subject><subject>Original Article</subject><subject>Plates (structural members)</subject><subject>Quadrilaterals</subject><subject>Sheets</subject><subject>Systems Theory</subject><subject>Two dimensional analysis</subject><subject>Vibration analysis</subject><subject>Vibration response</subject><issn>0177-0667</issn><issn>1435-5663</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kM1OwzAQhC0EEqXwApwscTas49ipj6jiT6rUC5wtx163qdKk2AlV3p6UIHHjtKPdmdHqI-SWwz0HKB4SgFCKQQYMeCaB8TMy47mQTColzskMeFEwUKq4JFcp7QC4ANAzMqwb2m2R1nbAeKwS0lA1VYcUa9xj09HQxn1f265qm5OmqRu1o7bxNERE-lWVcbraxtZDqhJtAw19405LW9cD3UTr0dM0Zo6V29LDWIfpmlwEWye8-Z1z8vH89L58Zav1y9vyccWc4LpjQmmvIXgshNRWYyY4aNQeSum8FMGJQpaZ9TwEJ9EtQil5KFSJPigvdS7m5G7qPcT2s8fUmV3bx_GzZLIil7leKHlyZZPLxTaliMEcYrW3cTAczAmxmRCbEbH5QWz4GBJTKI3mZoPxr_qf1DdwJ4Hk</recordid><startdate>20221201</startdate><enddate>20221201</enddate><creator>Hirane, Hicham</creator><creator>Belarbi, Mohamed-Ouejdi</creator><creator>Houari, Mohammed Sid Ahmed</creator><creator>Tounsi, Abdelouahed</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>PRINS</scope><scope>PTHSS</scope><scope>Q9U</scope><orcidid>https://orcid.org/0000-0002-5268-9925</orcidid></search><sort><creationdate>20221201</creationdate><title>On the layerwise finite element formulation for static and free vibration analysis of functionally graded sandwich plates</title><author>Hirane, Hicham ; Belarbi, Mohamed-Ouejdi ; Houari, Mohammed Sid Ahmed ; Tounsi, Abdelouahed</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-369d90fde7359a9e23109e9d0b5cd53fc375b2ad1ffc5ec8fb51f76bedf6d5943</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>CAE) and Design</topic><topic>Calculus of Variations and Optimal Control; Optimization</topic><topic>Classical Mechanics</topic><topic>Composite structures</topic><topic>Computer Science</topic><topic>Computer-Aided Engineering (CAD</topic><topic>Control</topic><topic>Displacement</topic><topic>Equations of motion</topic><topic>Exact solutions</topic><topic>Finite element method</topic><topic>Free vibration</topic><topic>Functionally gradient materials</topic><topic>Hamilton's principle</topic><topic>Material properties</topic><topic>Math. Applications in Chemistry</topic><topic>Mathematical and Computational Engineering</topic><topic>Mathematical models</topic><topic>Multilayers</topic><topic>Original Article</topic><topic>Plates (structural members)</topic><topic>Quadrilaterals</topic><topic>Sheets</topic><topic>Systems Theory</topic><topic>Two dimensional analysis</topic><topic>Vibration analysis</topic><topic>Vibration response</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hirane, Hicham</creatorcontrib><creatorcontrib>Belarbi, Mohamed-Ouejdi</creatorcontrib><creatorcontrib>Houari, Mohammed Sid Ahmed</creatorcontrib><creatorcontrib>Tounsi, Abdelouahed</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 Korea</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>ProQuest Central China</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>Hirane, Hicham</au><au>Belarbi, Mohamed-Ouejdi</au><au>Houari, Mohammed Sid Ahmed</au><au>Tounsi, Abdelouahed</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>On the layerwise finite element formulation for static and free vibration analysis of functionally graded sandwich plates</atitle><jtitle>Engineering with computers</jtitle><stitle>Engineering with Computers</stitle><date>2022-12-01</date><risdate>2022</risdate><volume>38</volume><issue>Suppl 5</issue><spage>3871</spage><epage>3899</epage><pages>3871-3899</pages><issn>0177-0667</issn><eissn>1435-5663</eissn><abstract>This paper presents a novel C
0
higher-order layerwise finite element model for static and free vibration analysis of functionally graded materials (FGM) sandwich plates. The proposed layerwise model, which is developed for multilayer composite plates, supposes higher-order displacement field for the core and first-order displacement field for the face sheets maintaining a continuity of displacement at layer. Unlike the conventional layerwise models, the present one has an important feature that the number of variables is fixed and does not increase when increasing the number of layers. Thus, based on the suggested model, a computationally efficient C
0
eight-node quadrilateral element is developed. Indeed, the new element is free of shear locking phenomenon without requiring any shear correction factors. Three common types of FGM plates, namely, (i) isotropic FGM plates; (ii) sandwich plates with FGM face sheets and homogeneous core and (iii) sandwich plates with homogeneous face sheets and FGM core, are considered in the present work. Material properties are assumed graded in the thickness direction according to a simple power law distribution in terms of the volume power laws of the constituents. The equations of motion of the FGM sandwich plate are obtained via the classical Hamilton’s principle. Numerical results of present model are compared with 2D, quasi-3D, and 3D analytical solutions and other predicted by advanced finite element models reported in the literature. The results indicate that the developed finite element model is promising in terms of accuracy and fast rate of convergence for both thin and thick FGM sandwich plates. Finally, it can be concluded that the proposed model is accurate and efficient in predicting the bending and free vibration responses of FGM sandwich plates.</abstract><cop>London</cop><pub>Springer London</pub><doi>10.1007/s00366-020-01250-1</doi><tpages>29</tpages><orcidid>https://orcid.org/0000-0002-5268-9925</orcidid></addata></record> |
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subjects | CAE) and Design Calculus of Variations and Optimal Control Optimization Classical Mechanics Composite structures Computer Science Computer-Aided Engineering (CAD Control Displacement Equations of motion Exact solutions Finite element method Free vibration Functionally gradient materials Hamilton's principle Material properties Math. Applications in Chemistry Mathematical and Computational Engineering Mathematical models Multilayers Original Article Plates (structural members) Quadrilaterals Sheets Systems Theory Two dimensional analysis Vibration analysis Vibration response |
title | On the layerwise finite element formulation for static and free vibration analysis of functionally graded sandwich plates |
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