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    Thin‐Walled Multicell Box‐Girder Finite Element

    Source: Journal of Structural Engineering:;1991:;Volume ( 117 ):;issue: 010
    Author:
    A. Ghani Razaqpur
    ,
    Hangang Li
    DOI: 10.1061/(ASCE)0733-9445(1991)117:10(2953)
    Publisher: American Society of Civil Engineers
    Abstract: A thin‐walled‐box‐girder finite element that can model extension, flexure, torsion, torsional warping, distortion, distortional warping, and shear lag effects was developed using an extended version of Vlasov's thin‐walled beam theory. The element has two end nodes, but it has besides the six nodal degrees of freedom of a conventional beam element, additional degrees of freedom to account for torsional warping, distortion, distortional warping, and shear lag. The governing differential equation pertaining to each action was used to derive the exact shape functions and the stiffness matrix and nodal load vector of the element. An orthogonalization procedure was employed to uncouple the various distortional and shear lag modes. A numerical example was solved that compared the proposed method with the facet‐shell finite element analysis, with good agreement between the two sets of results.
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      Thin‐Walled Multicell Box‐Girder Finite Element

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    contributor authorA. Ghani Razaqpur
    contributor authorHangang Li
    date accessioned2017-05-08T20:53:57Z
    date available2017-05-08T20:53:57Z
    date copyrightOctober 1991
    date issued1991
    identifier other%28asce%290733-9445%281991%29117%3A10%282953%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/30977
    description abstractA thin‐walled‐box‐girder finite element that can model extension, flexure, torsion, torsional warping, distortion, distortional warping, and shear lag effects was developed using an extended version of Vlasov's thin‐walled beam theory. The element has two end nodes, but it has besides the six nodal degrees of freedom of a conventional beam element, additional degrees of freedom to account for torsional warping, distortion, distortional warping, and shear lag. The governing differential equation pertaining to each action was used to derive the exact shape functions and the stiffness matrix and nodal load vector of the element. An orthogonalization procedure was employed to uncouple the various distortional and shear lag modes. A numerical example was solved that compared the proposed method with the facet‐shell finite element analysis, with good agreement between the two sets of results.
    publisherAmerican Society of Civil Engineers
    titleThin‐Walled Multicell Box‐Girder Finite Element
    typeJournal Paper
    journal volume117
    journal issue10
    journal titleJournal of Structural Engineering
    identifier doi10.1061/(ASCE)0733-9445(1991)117:10(2953)
    treeJournal of Structural Engineering:;1991:;Volume ( 117 ):;issue: 010
    contenttypeFulltext
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