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    Assessment of Inverse Hyperbolic Zigzag Theory for Hygro-Thermomechanical Analysis of Laminated Composite and Sandwich Plates

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    Author:
    Nikhil Garg
    ,
    Karkhanis Rahul Sanjay
    ,
    Rosalin Sahoo
    ,
    P. R. Maiti
    ,
    B. N. Singh
    DOI: 10.1061/(ASCE)AS.1943-5525.0001177
    Publisher: ASCE
    Abstract: In the present work, the hygro-thermomechanical response on the static characteristics of symmetric and antisymmetric laminated composite and sandwich plates is obtained using the recently developed inverse hyperbolic zigzag theory (IHZZT). The framework of IHZZT inculcates the shear strain shape function assuming a nonlinear distribution of transverse shear stresses. It satisfies the necessary conditions of interlaminar stress continuity at the layer interfaces as well as the condition of zero transverse shear stresses at the top and bottom surfaces of the plates. The theory has seven unknown field variables, which are layer-independent. The displacement-based finite-element approach is employed, using the eight-noded isoparametric serendipity element, accounting for the C0 continuity. A number of numerical examples are solved considering the effect of temperature, moisture concentration, span-thickness ratio, aspect ratio, boundary conditions, loading conditions, and variations in the number of layers. The results obtained in terms of deflections and stresses are validated with the exact results and results available in the existing literature. A few new results are produced here to establish a benchmark study for future research.
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      Assessment of Inverse Hyperbolic Zigzag Theory for Hygro-Thermomechanical Analysis of Laminated Composite and Sandwich Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4268653
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    contributor authorNikhil Garg
    contributor authorKarkhanis Rahul Sanjay
    contributor authorRosalin Sahoo
    contributor authorP. R. Maiti
    contributor authorB. N. Singh
    date accessioned2022-01-30T21:40:50Z
    date available2022-01-30T21:40:50Z
    date issued9/1/2020 12:00:00 AM
    identifier other%28ASCE%29AS.1943-5525.0001177.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4268653
    description abstractIn the present work, the hygro-thermomechanical response on the static characteristics of symmetric and antisymmetric laminated composite and sandwich plates is obtained using the recently developed inverse hyperbolic zigzag theory (IHZZT). The framework of IHZZT inculcates the shear strain shape function assuming a nonlinear distribution of transverse shear stresses. It satisfies the necessary conditions of interlaminar stress continuity at the layer interfaces as well as the condition of zero transverse shear stresses at the top and bottom surfaces of the plates. The theory has seven unknown field variables, which are layer-independent. The displacement-based finite-element approach is employed, using the eight-noded isoparametric serendipity element, accounting for the C0 continuity. A number of numerical examples are solved considering the effect of temperature, moisture concentration, span-thickness ratio, aspect ratio, boundary conditions, loading conditions, and variations in the number of layers. The results obtained in terms of deflections and stresses are validated with the exact results and results available in the existing literature. A few new results are produced here to establish a benchmark study for future research.
    publisherASCE
    titleAssessment of Inverse Hyperbolic Zigzag Theory for Hygro-Thermomechanical Analysis of Laminated Composite and Sandwich Plates
    typeJournal Paper
    journal volume33
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001177
    page16
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    contenttypeFulltext
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