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    Assessment and Accuracy of New Nonpolynomial Shear Deformation Theories for Static Analysis of Laminated and Braided Composite Plates

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author:
    Durgesh Bahadur Singh
    ,
    B. N. Singh
    DOI: 10.1061/(ASCE)AS.1943-5525.0000768
    Publisher: American Society of Civil Engineers
    Abstract: In the present study, two new shear deformation theories, trigonometric deformation theory (TDT) and trigonometric-hyperbolic deformation theory (THDT), are proposed. These theories are examined in detail for their effectiveness in static response of laminated and three-dimensional (3D) braided composite plates. Both models are based upon a shear strain shape function that yields nonlinear distribution of transverse shear stresses and also satisfies the traction-free boundary conditions on top and bottom surfaces of the plate. Thus, requirement of shear correction factor vanishes. Virtual work principle is used to obtain the governing differential equations and boundary conditions. These models are formulated and validated for the static responses of laminated and braided composite plates. A variety of numerical examples are analyzed. Comparison of various higher order theories with the proposed theories are performed. It is observed that both proposed theories are efficient and accurate for the static analysis of laminated and 3D braided composite plates. Intensive numerical studies of 3D braided composite are performed in detail. It is further observed that the geometric parameter (aspect ratio), boundary condition, fiber volume fraction, and braiding angle have a significant effect on the static response of the braided composite plates. In the framework of finite element analysis, both proposed theories anticipate exemplary results for the laminated and braided composite plates compared to existing theories.
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      Assessment and Accuracy of New Nonpolynomial Shear Deformation Theories for Static Analysis of Laminated and Braided Composite Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4245049
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    contributor authorDurgesh Bahadur Singh
    contributor authorB. N. Singh
    date accessioned2017-12-30T13:03:07Z
    date available2017-12-30T13:03:07Z
    date issued2017
    identifier other%28ASCE%29AS.1943-5525.0000768.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4245049
    description abstractIn the present study, two new shear deformation theories, trigonometric deformation theory (TDT) and trigonometric-hyperbolic deformation theory (THDT), are proposed. These theories are examined in detail for their effectiveness in static response of laminated and three-dimensional (3D) braided composite plates. Both models are based upon a shear strain shape function that yields nonlinear distribution of transverse shear stresses and also satisfies the traction-free boundary conditions on top and bottom surfaces of the plate. Thus, requirement of shear correction factor vanishes. Virtual work principle is used to obtain the governing differential equations and boundary conditions. These models are formulated and validated for the static responses of laminated and braided composite plates. A variety of numerical examples are analyzed. Comparison of various higher order theories with the proposed theories are performed. It is observed that both proposed theories are efficient and accurate for the static analysis of laminated and 3D braided composite plates. Intensive numerical studies of 3D braided composite are performed in detail. It is further observed that the geometric parameter (aspect ratio), boundary condition, fiber volume fraction, and braiding angle have a significant effect on the static response of the braided composite plates. In the framework of finite element analysis, both proposed theories anticipate exemplary results for the laminated and braided composite plates compared to existing theories.
    publisherAmerican Society of Civil Engineers
    titleAssessment and Accuracy of New Nonpolynomial Shear Deformation Theories for Static Analysis of Laminated and Braided Composite Plates
    typeJournal Paper
    journal volume30
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000768
    page04017056
    treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    contenttypeFulltext
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