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    Mixed Finite-Element Formulation Based on Refined Sinusoidal Model for Buckling of Layered Beams

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
    Author:
    Ren Xiaohui
    ,
    Wu Zhen
    DOI: 10.1061/(ASCE)AS.1943-5525.0001125
    Publisher: ASCE
    Abstract: In the last 3 decades, sinusoidal theory has been increasingly utilized to research mechanical behaviors of layered composite and sandwich structures. Nevertheless, the existing sinusoidal model will encounter trouble in precisely yielding the buckling loads of layered structures composed of layers with different material properties. Thus, a refined sinusoidal model is offered for the buckling analysis of composite and sandwich structures that can simulate the zigzag effect of the in-plane displacement and meet the free conditions of transverse shear stresses on the surfaces. In the light of the elegant sinusoidal model, a three-node beam element has been constructed to work out the discrete eigenvalue equation coming from the stability behavior. Making use of a mixed variational theorem from the literature, the finite-element formulation can meet beforehand the continuous conditions of transverse stress at the interfaces. The three-dimensional finite element method (3D-FEM) results are utilized to evaluate the precision and efficiency of the proposed approach through a numerical example. The proposed finite-element formulation can produce satisfactory results with lower calculational cost, and some interesting conclusions are presented. However, the results for stability of layered structures made of plies with different material properties will be overestimated by utilizing the models violating the continuous prerequisite of interlaminar stresses.
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      Mixed Finite-Element Formulation Based on Refined Sinusoidal Model for Buckling of Layered Beams

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4266595
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    contributor authorRen Xiaohui
    contributor authorWu Zhen
    date accessioned2022-01-30T20:08:51Z
    date available2022-01-30T20:08:51Z
    date issued2020
    identifier other%28ASCE%29AS.1943-5525.0001125.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4266595
    description abstractIn the last 3 decades, sinusoidal theory has been increasingly utilized to research mechanical behaviors of layered composite and sandwich structures. Nevertheless, the existing sinusoidal model will encounter trouble in precisely yielding the buckling loads of layered structures composed of layers with different material properties. Thus, a refined sinusoidal model is offered for the buckling analysis of composite and sandwich structures that can simulate the zigzag effect of the in-plane displacement and meet the free conditions of transverse shear stresses on the surfaces. In the light of the elegant sinusoidal model, a three-node beam element has been constructed to work out the discrete eigenvalue equation coming from the stability behavior. Making use of a mixed variational theorem from the literature, the finite-element formulation can meet beforehand the continuous conditions of transverse stress at the interfaces. The three-dimensional finite element method (3D-FEM) results are utilized to evaluate the precision and efficiency of the proposed approach through a numerical example. The proposed finite-element formulation can produce satisfactory results with lower calculational cost, and some interesting conclusions are presented. However, the results for stability of layered structures made of plies with different material properties will be overestimated by utilizing the models violating the continuous prerequisite of interlaminar stresses.
    publisherASCE
    titleMixed Finite-Element Formulation Based on Refined Sinusoidal Model for Buckling of Layered Beams
    typeJournal Paper
    journal volume33
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001125
    page04020030
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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