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    Vibration of Laminate-Faced Sandwich Plate by a New Refined Element

    Source: Journal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003
    Author:
    A. Chakrabarti
    ,
    A. H. Sheikh
    DOI: 10.1061/(ASCE)0893-1321(2004)17:3(123)
    Publisher: American Society of Civil Engineers
    Abstract: An efficient six-noded triangular element based on refined plate theory is developed for the analysis of sandwich plates with stiff laminated face sheets and it is applied to a free vibration problem in this paper. The plate theory represents parabolic through thickness variation of transverse shear stresses with continuity at the layer interfaces, which introduces discontinuity at these interfaces for the shear strains. It is to be noted that the plate theory requires unknowns at the reference plane only. Moreover, it ensures a shear stress-free condition at the top and bottom surfaces of the plate. Thus, the plate theory has all of the features required for an accurate modeling of laminated sandwich plates. The plate theory suffers from a problem in its finite element implementation since it requires
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      Vibration of Laminate-Faced Sandwich Plate by a New Refined Element

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    http://yetl.yabesh.ir/yetl1/handle/yetl/45006
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    contributor authorA. Chakrabarti
    contributor authorA. H. Sheikh
    date accessioned2017-05-08T21:16:10Z
    date available2017-05-08T21:16:10Z
    date copyrightJuly 2004
    date issued2004
    identifier other%28asce%290893-1321%282004%2917%3A3%28123%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45006
    description abstractAn efficient six-noded triangular element based on refined plate theory is developed for the analysis of sandwich plates with stiff laminated face sheets and it is applied to a free vibration problem in this paper. The plate theory represents parabolic through thickness variation of transverse shear stresses with continuity at the layer interfaces, which introduces discontinuity at these interfaces for the shear strains. It is to be noted that the plate theory requires unknowns at the reference plane only. Moreover, it ensures a shear stress-free condition at the top and bottom surfaces of the plate. Thus, the plate theory has all of the features required for an accurate modeling of laminated sandwich plates. The plate theory suffers from a problem in its finite element implementation since it requires
    publisherAmerican Society of Civil Engineers
    titleVibration of Laminate-Faced Sandwich Plate by a New Refined Element
    typeJournal Paper
    journal volume17
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2004)17:3(123)
    treeJournal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003
    contenttypeFulltext
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