Suggestion of Analytical Method of Three-Dimensional Stress Analysis for Laminated Composite Structures
It is well known that the mechanical properties of laminated composites depend on the stacking sequences. As the bending modulus of elasticity is affected remarkably by the stacking sequences, the stress and strain analyses for laminated composite structures require a special technique. Therefore, a...
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Veröffentlicht in: | Journal of the Society of Materials Science, Japan Japan, 1995/04/15, Vol.44(499), pp.390-394 |
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creator | ZAKO, Masaru TSUJIKAMI, Tetsuya KITAMURA, Takanori |
description | It is well known that the mechanical properties of laminated composites depend on the stacking sequences. As the bending modulus of elasticity is affected remarkably by the stacking sequences, the stress and strain analyses for laminated composite structures require a special technique. Therefore, a new analytical method has been proposed in order to calculate the mechanical behavior of laminated structures in this paper. The proposed method has been applied for a laminated composite structure as a numerical example. As a result, it has been recognized that the numerical behavior of the composite structure with anisotropic properties under mixed loads of bending and tension can be analyzed by the proposed method, even if it has two different moduli of elasticity of bending and tension. In addition, CPU time of FEM based on the proposed method can be reduced remarkably as compared with ordinary FEM. |
doi_str_mv | 10.2472/jsms.44.390 |
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As the bending modulus of elasticity is affected remarkably by the stacking sequences, the stress and strain analyses for laminated composite structures require a special technique. Therefore, a new analytical method has been proposed in order to calculate the mechanical behavior of laminated structures in this paper. The proposed method has been applied for a laminated composite structure as a numerical example. As a result, it has been recognized that the numerical behavior of the composite structure with anisotropic properties under mixed loads of bending and tension can be analyzed by the proposed method, even if it has two different moduli of elasticity of bending and tension. In addition, CPU time of FEM based on the proposed method can be reduced remarkably as compared with ordinary FEM.</description><identifier>ISSN: 0514-5163</identifier><identifier>EISSN: 1880-7488</identifier><identifier>DOI: 10.2472/jsms.44.390</identifier><identifier>CODEN: ZARYAQ</identifier><language>eng ; jpn</language><publisher>Kyoto: The Society of Materials Science, Japan</publisher><subject>Anisotropy ; Composites ; Fracture ; Laminate ; Stress analysis ; Three-Dimensional FEM</subject><ispartof>Journal of the Society of Materials Science, Japan, 1995/04/15, Vol.44(499), pp.390-394</ispartof><rights>by The Society of Materials Science, Japan</rights><rights>1995 INIST-CNRS</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,1883,4024,27923,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3565057$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>ZAKO, Masaru</creatorcontrib><creatorcontrib>TSUJIKAMI, Tetsuya</creatorcontrib><creatorcontrib>KITAMURA, Takanori</creatorcontrib><title>Suggestion of Analytical Method of Three-Dimensional Stress Analysis for Laminated Composite Structures</title><title>Journal of the Society of Materials Science, Japan</title><addtitle>J. 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In addition, CPU time of FEM based on the proposed method can be reduced remarkably as compared with ordinary FEM.</description><subject>Anisotropy</subject><subject>Composites</subject><subject>Fracture</subject><subject>Laminate</subject><subject>Stress analysis</subject><subject>Three-Dimensional FEM</subject><issn>0514-5163</issn><issn>1880-7488</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1995</creationdate><recordtype>article</recordtype><recordid>eNqN0L1u2zAUBWAiaIEYSaa-gIYgSyGXv6I4Bm7TFHDRIelM0NSlzUASXV5pyNuHqlPPnQjwfjzEPYR8YnTNpeZfXnDAtZRrYegFWbG2pbWWbfuBrKhislasEZfkBjHuKOWci1aaFdk_zfs94BTTWKVQ3Y-uf52id331E6ZD6pbL50MGqL_GAUYsrsyepgyIJ40Rq5BytXVDHN0EXbVJwzFhnGBxs5_mgq_Jx-B6hJv384r8fvj2vHmst7--_9jcb2svlKS1CbLRHYSG6WAa6Znj1HVlPdE5LuXOKyeUbkxQigm9E52kQoBhfueDot6LK3J3yj3m9Gcui9khooe-dyOkGS1XpuWNUf8DtTaUFfj5BH1OiBmCPeY4uPxqGbVL8XYp3kppS_FF377HOiwthuxGH_H8RKhGUaULezyxF5zcHs5zl0v5PfyNZKYRS6w05t9RfjgTf3DZwijeADOlnac</recordid><startdate>1995</startdate><enddate>1995</enddate><creator>ZAKO, Masaru</creator><creator>TSUJIKAMI, Tetsuya</creator><creator>KITAMURA, Takanori</creator><general>The Society of Materials Science, Japan</general><general>Society of Materials Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7SR</scope><scope>JG9</scope></search><sort><creationdate>1995</creationdate><title>Suggestion of Analytical Method of Three-Dimensional Stress Analysis for Laminated Composite Structures</title><author>ZAKO, Masaru ; TSUJIKAMI, Tetsuya ; KITAMURA, Takanori</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3540-9f467def617f964c1a20ad2473da244bc5a35769f55137b3d4033e91cbcf50cc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng ; jpn</language><creationdate>1995</creationdate><topic>Anisotropy</topic><topic>Composites</topic><topic>Fracture</topic><topic>Laminate</topic><topic>Stress analysis</topic><topic>Three-Dimensional FEM</topic><toplevel>online_resources</toplevel><creatorcontrib>ZAKO, Masaru</creatorcontrib><creatorcontrib>TSUJIKAMI, Tetsuya</creatorcontrib><creatorcontrib>KITAMURA, Takanori</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Engineered Materials Abstracts</collection><collection>Materials Research Database</collection><jtitle>Journal of the Society of Materials Science, Japan</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>ZAKO, Masaru</au><au>TSUJIKAMI, Tetsuya</au><au>KITAMURA, Takanori</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Suggestion of Analytical Method of Three-Dimensional Stress Analysis for Laminated Composite Structures</atitle><jtitle>Journal of the Society of Materials Science, Japan</jtitle><addtitle>J. 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As a result, it has been recognized that the numerical behavior of the composite structure with anisotropic properties under mixed loads of bending and tension can be analyzed by the proposed method, even if it has two different moduli of elasticity of bending and tension. In addition, CPU time of FEM based on the proposed method can be reduced remarkably as compared with ordinary FEM.</abstract><cop>Kyoto</cop><pub>The Society of Materials Science, Japan</pub><doi>10.2472/jsms.44.390</doi><tpages>5</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Anisotropy Composites Fracture Laminate Stress analysis Three-Dimensional FEM |
title | Suggestion of Analytical Method of Three-Dimensional Stress Analysis for Laminated Composite Structures |
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