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    Free Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
    Author:
    Pratik Tiwari
    ,
    Swarup K. Barman
    ,
    Dipak K. Maiti
    ,
    Damodar Maity
    DOI: 10.1061/(ASCE)AS.1943-5525.0001053
    Publisher: American Society of Civil Engineers
    Abstract: In this study, a new model for analyzing delaminated plates was developed using three-dimensional (3D) degenerated elements. The elements were developed using the degenerated solid approach based on Reissner-Mindlin assumptions. Thus, the shear deformation and rotary inertia effect were considered, and the 3D field was reduced to a two-dimensional (2D) field in terms of midsurface nodal variables. The delamination was incorporated using Heaviside step functions. The proposed model was found to be very accurate and also faster in comparison with layerwise/higher-order theories. Results for natural frequencies of plates and beams with and without delamination were compared with theoretical and experimental results available in the literature and were in excellent agreement. New results were generated using the proposed method for different boundary conditions, ply orientations, size of delamination, and location of delamination; these will serve as benchmarks for future research.
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      Free Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4260196
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    contributor authorPratik Tiwari
    contributor authorSwarup K. Barman
    contributor authorDipak K. Maiti
    contributor authorDamodar Maity
    date accessioned2019-09-18T10:40:48Z
    date available2019-09-18T10:40:48Z
    date issued2019
    identifier other%28ASCE%29AS.1943-5525.0001053.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4260196
    description abstractIn this study, a new model for analyzing delaminated plates was developed using three-dimensional (3D) degenerated elements. The elements were developed using the degenerated solid approach based on Reissner-Mindlin assumptions. Thus, the shear deformation and rotary inertia effect were considered, and the 3D field was reduced to a two-dimensional (2D) field in terms of midsurface nodal variables. The delamination was incorporated using Heaviside step functions. The proposed model was found to be very accurate and also faster in comparison with layerwise/higher-order theories. Results for natural frequencies of plates and beams with and without delamination were compared with theoretical and experimental results available in the literature and were in excellent agreement. New results were generated using the proposed method for different boundary conditions, ply orientations, size of delamination, and location of delamination; these will serve as benchmarks for future research.
    publisherAmerican Society of Civil Engineers
    titleFree Vibration Analysis of Delaminated Composite Plate Using 3D Degenerated Element
    typeJournal Paper
    journal volume32
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001053
    page04019070
    treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
    contenttypeFulltext
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