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    Designing a Stiffener Layout that Resists the Wrinkling Behaviors of Sandwich Panels

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005::page 04024067-1
    Author:
    Zhen Wu
    ,
    Senlin Zhang
    DOI: 10.1061/JAEEEZ.ASENG-5575
    Publisher: American Society of Civil Engineers
    Abstract: Wrinkling is a typical failure mode of sandwich structures with thin skins, where the bending deformation of face skins occurs simultaneously in conjunction with transverse stretching deformation of core layer. To analyze the three-dimensional (3D) deformation of wrinkling, a model is required to possess a capability describing completely different deformations at each ply. Therefore, by utilizing the Chebyshev polynomial at each layer of sandwich panels, this paper focuses on proposing a higher-order model to individually illustrate deformations of the skins and the core. By means of the proposed model, a refined triangular element has been constructed. By analyzing the stability of a sandwich plate without stiffeners, the finite-element formulation has been verified by comparing it to the quasi-3D elasticity solutions. In addition, it is anticipated that wrinkling failure can be effectively restrained by designing the stiffener layout. To this end, the influence of stiffener layouts on wrinkling behaviors of sandwich plates has been investigated in detail, and it is found that the capability of resisting the wrinkling deformation can be obviously improved by designing reasonable stiffener layouts. Moreover, the translation between buckling and wrinkling behaviors of sandwich panels with different stiffeners has been also explored, which can help to better understand wrinkling deformation mechanism. In summary, the proposed model can be used to design a reasonable arrangement of stiffeners to resist the wrinkling failure of sandwich panels.
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      Designing a Stiffener Layout that Resists the Wrinkling Behaviors of Sandwich Panels

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    contributor authorZhen Wu
    contributor authorSenlin Zhang
    date accessioned2024-12-24T10:15:07Z
    date available2024-12-24T10:15:07Z
    date copyright9/1/2024 12:00:00 AM
    date issued2024
    identifier otherJAEEEZ.ASENG-5575.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4298573
    description abstractWrinkling is a typical failure mode of sandwich structures with thin skins, where the bending deformation of face skins occurs simultaneously in conjunction with transverse stretching deformation of core layer. To analyze the three-dimensional (3D) deformation of wrinkling, a model is required to possess a capability describing completely different deformations at each ply. Therefore, by utilizing the Chebyshev polynomial at each layer of sandwich panels, this paper focuses on proposing a higher-order model to individually illustrate deformations of the skins and the core. By means of the proposed model, a refined triangular element has been constructed. By analyzing the stability of a sandwich plate without stiffeners, the finite-element formulation has been verified by comparing it to the quasi-3D elasticity solutions. In addition, it is anticipated that wrinkling failure can be effectively restrained by designing the stiffener layout. To this end, the influence of stiffener layouts on wrinkling behaviors of sandwich plates has been investigated in detail, and it is found that the capability of resisting the wrinkling deformation can be obviously improved by designing reasonable stiffener layouts. Moreover, the translation between buckling and wrinkling behaviors of sandwich panels with different stiffeners has been also explored, which can help to better understand wrinkling deformation mechanism. In summary, the proposed model can be used to design a reasonable arrangement of stiffeners to resist the wrinkling failure of sandwich panels.
    publisherAmerican Society of Civil Engineers
    titleDesigning a Stiffener Layout that Resists the Wrinkling Behaviors of Sandwich Panels
    typeJournal Article
    journal volume37
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5575
    journal fristpage04024067-1
    journal lastpage04024067-12
    page12
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005
    contenttypeFulltext
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