Generalized Free-Edge Stress Analysis Using Mechanics of Structure Genome
This work reveals the potential of mechanics of structure genome (MSG) for the free-edge stress analysis of composite laminates. First, the cross-sectional analysis specialized from MSG is formulated for solving a generalized free-edge problem of composite laminates. Then, MSG and the companion code...
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| Veröffentlicht in: | Journal of applied mechanics 2016-10, Vol.83 (10) |
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| container_title | Journal of applied mechanics |
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| creator | Peng, Bo Goodsell, Johnathan Byron Pipes, R Yu, Wenbin |
| description | This work reveals the potential of mechanics of structure genome (MSG) for the free-edge stress analysis of composite laminates. First, the cross-sectional analysis specialized from MSG is formulated for solving a generalized free-edge problem of composite laminates. Then, MSG and the companion code SwiftComp™ are applied to the free-edge stress analysis of several composite laminates with arbitrary layups and general loads including extension, torsion, in-plane and out-of-plane bending, and their combinations. The results of MSG are compared with various existing solutions for symmetric angle-ply laminates. New results are presented for the free-edge stress fields in general laminates for combined mechanical loads and compared with three-dimensional (3D) finite element analysis (FEA) results, which agree very well. |
| doi_str_mv | 10.1115/1.4034389 |
| format | Article |
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First, the cross-sectional analysis specialized from MSG is formulated for solving a generalized free-edge problem of composite laminates. Then, MSG and the companion code SwiftComp™ are applied to the free-edge stress analysis of several composite laminates with arbitrary layups and general loads including extension, torsion, in-plane and out-of-plane bending, and their combinations. The results of MSG are compared with various existing solutions for symmetric angle-ply laminates. New results are presented for the free-edge stress fields in general laminates for combined mechanical loads and compared with three-dimensional (3D) finite element analysis (FEA) results, which agree very well.</description><identifier>ISSN: 0021-8936</identifier><identifier>EISSN: 1528-9036</identifier><identifier>DOI: 10.1115/1.4034389</identifier><language>eng</language><publisher>ASME</publisher><subject>Bending ; Cross sections ; Finite element method ; Genomes ; Laminates ; Mathematical analysis ; Stress analysis ; Torsion</subject><ispartof>Journal of applied mechanics, 2016-10, Vol.83 (10)</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a282t-45cf5bc9047877c00980125b97f3d5f7636f70bac4a5aba55323408edc7fe8f3</citedby><cites>FETCH-LOGICAL-a282t-45cf5bc9047877c00980125b97f3d5f7636f70bac4a5aba55323408edc7fe8f3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,778,782,27907,27908,38503</link.rule.ids></links><search><creatorcontrib>Peng, Bo</creatorcontrib><creatorcontrib>Goodsell, Johnathan</creatorcontrib><creatorcontrib>Byron Pipes, R</creatorcontrib><creatorcontrib>Yu, Wenbin</creatorcontrib><title>Generalized Free-Edge Stress Analysis Using Mechanics of Structure Genome</title><title>Journal of applied mechanics</title><addtitle>J. Appl. Mech</addtitle><description>This work reveals the potential of mechanics of structure genome (MSG) for the free-edge stress analysis of composite laminates. First, the cross-sectional analysis specialized from MSG is formulated for solving a generalized free-edge problem of composite laminates. Then, MSG and the companion code SwiftComp™ are applied to the free-edge stress analysis of several composite laminates with arbitrary layups and general loads including extension, torsion, in-plane and out-of-plane bending, and their combinations. The results of MSG are compared with various existing solutions for symmetric angle-ply laminates. 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Appl. Mech</stitle><date>2016-10-01</date><risdate>2016</risdate><volume>83</volume><issue>10</issue><issn>0021-8936</issn><eissn>1528-9036</eissn><abstract>This work reveals the potential of mechanics of structure genome (MSG) for the free-edge stress analysis of composite laminates. First, the cross-sectional analysis specialized from MSG is formulated for solving a generalized free-edge problem of composite laminates. Then, MSG and the companion code SwiftComp™ are applied to the free-edge stress analysis of several composite laminates with arbitrary layups and general loads including extension, torsion, in-plane and out-of-plane bending, and their combinations. The results of MSG are compared with various existing solutions for symmetric angle-ply laminates. New results are presented for the free-edge stress fields in general laminates for combined mechanical loads and compared with three-dimensional (3D) finite element analysis (FEA) results, which agree very well.</abstract><pub>ASME</pub><doi>10.1115/1.4034389</doi></addata></record> |
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| language | eng |
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| source | ASME Transactions Journals (Current); Alma/SFX Local Collection |
| subjects | Bending Cross sections Finite element method Genomes Laminates Mathematical analysis Stress analysis Torsion |
| title | Generalized Free-Edge Stress Analysis Using Mechanics of Structure Genome |
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