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    New Sinusoidal Higher-Order Theory Including the Zig-Zag Function for Multilayered Composite Beams

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 003
    Author:
    Donglin Zhao; Zhen Wu; Xiaohui Ren
    DOI: 10.1061/(ASCE)AS.1943-5525.0000994
    Publisher: American Society of Civil Engineers
    Abstract: With the advantage of satisfying zero shear stress conditions on surfaces, the sinusoidal theory has been widely used for static and dynamic analysis of composite laminated structures. Nevertheless, sinusoidal theories accounting for zig-zag effects have hitherto rarely been reported in the literature because zero shear stress conditions on the surfaces will be violated once the existing zig-zag function is taken into account. Thus, a new zig-zag function that can satisfy traction-free boundary conditions has been developed in this paper. Introducing the developed zig-zag function into the sinusoidal model, a new sinusoidal shear deformation beam theory including the zig-zag function has been proposed, which can accurately describe the zig-zag effect. Other higher-order theories and the first-order theory proposed by other investigators are also considered for the evaluation. By investigating the typical bending problems of multilayer beams, comparison of the present results with three-dimensional elasticity solutions and the results obtained independently using other models shows that the proposed model can more precisely produce the displacements and stresses of laminated composite and sandwich beams in comparison with other models considered in this article.
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      New Sinusoidal Higher-Order Theory Including the Zig-Zag Function for Multilayered Composite Beams

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4255194
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    contributor authorDonglin Zhao; Zhen Wu; Xiaohui Ren
    date accessioned2019-03-10T12:14:39Z
    date available2019-03-10T12:14:39Z
    date issued2019
    identifier other%28ASCE%29AS.1943-5525.0000994.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255194
    description abstractWith the advantage of satisfying zero shear stress conditions on surfaces, the sinusoidal theory has been widely used for static and dynamic analysis of composite laminated structures. Nevertheless, sinusoidal theories accounting for zig-zag effects have hitherto rarely been reported in the literature because zero shear stress conditions on the surfaces will be violated once the existing zig-zag function is taken into account. Thus, a new zig-zag function that can satisfy traction-free boundary conditions has been developed in this paper. Introducing the developed zig-zag function into the sinusoidal model, a new sinusoidal shear deformation beam theory including the zig-zag function has been proposed, which can accurately describe the zig-zag effect. Other higher-order theories and the first-order theory proposed by other investigators are also considered for the evaluation. By investigating the typical bending problems of multilayer beams, comparison of the present results with three-dimensional elasticity solutions and the results obtained independently using other models shows that the proposed model can more precisely produce the displacements and stresses of laminated composite and sandwich beams in comparison with other models considered in this article.
    publisherAmerican Society of Civil Engineers
    titleNew Sinusoidal Higher-Order Theory Including the Zig-Zag Function for Multilayered Composite Beams
    typeJournal Paper
    journal volume32
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000994
    page04019009
    treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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