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    Analysis of Thick Circular Plates Undergoing Large Deflections

    Source: Journal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 001
    Author:
    M. Gorji
    ,
    J. A. Abuyan
    ,
    K. S. Y. Li
    DOI: 10.1061/(ASCE)0893-1321(1992)5:1(138)
    Publisher: American Society of Civil Engineers
    Abstract: This investigation considers the effect of transverse shear deformation on bending of the axisymmetrically loaded isotropic and orthotropic circular and annular plates undergoing large deflection. The analysis treats the nonlinear terms of lateral displacement as fictitious loads acting on the plate. The solution of a von Kármán‐type plate is, therefore, reduced to a plane problem in elasticity and a linear plate‐bending problem. Results are presented for simply supported and clamped plates and are in good agreement with the available solutions. For plates considered in this study, the influence of shear deformation on lateral displacement becomes more significant as the orthotropic parameter increases. The linear and nonlinear solutions for orthotropic plates deviate at a low value of the maximum deflection‐to‐thickness ratio
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      Analysis of Thick Circular Plates Undergoing Large Deflections

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44719
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    • Journal of Aerospace Engineering

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    contributor authorM. Gorji
    contributor authorJ. A. Abuyan
    contributor authorK. S. Y. Li
    date accessioned2017-05-08T21:15:40Z
    date available2017-05-08T21:15:40Z
    date copyrightJanuary 1992
    date issued1992
    identifier other%28asce%290893-1321%281992%295%3A1%28138%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44719
    description abstractThis investigation considers the effect of transverse shear deformation on bending of the axisymmetrically loaded isotropic and orthotropic circular and annular plates undergoing large deflection. The analysis treats the nonlinear terms of lateral displacement as fictitious loads acting on the plate. The solution of a von Kármán‐type plate is, therefore, reduced to a plane problem in elasticity and a linear plate‐bending problem. Results are presented for simply supported and clamped plates and are in good agreement with the available solutions. For plates considered in this study, the influence of shear deformation on lateral displacement becomes more significant as the orthotropic parameter increases. The linear and nonlinear solutions for orthotropic plates deviate at a low value of the maximum deflection‐to‐thickness ratio
    publisherAmerican Society of Civil Engineers
    titleAnalysis of Thick Circular Plates Undergoing Large Deflections
    typeJournal Paper
    journal volume5
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1992)5:1(138)
    treeJournal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 001
    contenttypeFulltext
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