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    Rhombic Laminates with Mass Variations under Dual-Axis Compression

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 003
    Author:
    Anish
    ,
    Ajay Kumar
    ,
    Anupam Chakrabarti
    ,
    Marcin K. Widomski
    ,
    Danuta Barnat-Hunek
    DOI: 10.1061/(ASCE)AS.1943-5525.0001118
    Publisher: ASCE
    Abstract: Biaxial buckling of the laminated composite rhombic (skew) plate with mass variations in the form of openings and adding extra mass at the center of the plate was studied using improved shear deformation theory (ISDT). The ISDT mathematical model incorporates third-degree variation of the thickness coordinate in the displacement formulation. In the presented theory, the use of shear correction factor was eliminated and a second-order variation of transverse shear strains through the plate thickness was implied. A computer-based algorithm based on the C0 finite-element formulation of the mathematical model was developed to analyze the buckling behavior of a laminated composite skew plate with openings and extra mass imposed at the center of the plate. Due to a lack of results in the literature based on the ISDT of the considered problem of biaxial buckling of laminated composite skew plates with openings cutout and extra mass imposed at the center of plate, the present results were validated with the suitable results available for laminated composite plates without openings/extra mass imposed at the center of plate with zero skew angle. The new results were obtained by varying the geometry, boundary conditions, ply orientations, and skew angles.
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      Rhombic Laminates with Mass Variations under Dual-Axis Compression

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4266517
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    contributor authorAnish
    contributor authorAjay Kumar
    contributor authorAnupam Chakrabarti
    contributor authorMarcin K. Widomski
    contributor authorDanuta Barnat-Hunek
    date accessioned2022-01-30T20:05:59Z
    date available2022-01-30T20:05:59Z
    date issued2020
    identifier other%28ASCE%29AS.1943-5525.0001118.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4266517
    description abstractBiaxial buckling of the laminated composite rhombic (skew) plate with mass variations in the form of openings and adding extra mass at the center of the plate was studied using improved shear deformation theory (ISDT). The ISDT mathematical model incorporates third-degree variation of the thickness coordinate in the displacement formulation. In the presented theory, the use of shear correction factor was eliminated and a second-order variation of transverse shear strains through the plate thickness was implied. A computer-based algorithm based on the C0 finite-element formulation of the mathematical model was developed to analyze the buckling behavior of a laminated composite skew plate with openings and extra mass imposed at the center of the plate. Due to a lack of results in the literature based on the ISDT of the considered problem of biaxial buckling of laminated composite skew plates with openings cutout and extra mass imposed at the center of plate, the present results were validated with the suitable results available for laminated composite plates without openings/extra mass imposed at the center of plate with zero skew angle. The new results were obtained by varying the geometry, boundary conditions, ply orientations, and skew angles.
    publisherASCE
    titleRhombic Laminates with Mass Variations under Dual-Axis Compression
    typeJournal Paper
    journal volume33
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001118
    page04020013
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 003
    contenttypeFulltext
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