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    Cylindrical Buckling Load of Laminated Columns

    Source: Journal of Engineering Mechanics:;1989:;Volume ( 115 ):;issue: 003
    Author:
    Izhak Sheinman
    DOI: 10.1061/(ASCE)0733-9399(1989)115:3(659)
    Publisher: American Society of Civil Engineers
    Abstract: The cylindrical buckling load of a composite laminated column is derived from plate theory. The effect of lamina orientation is taken into account by treating the stiffness parameter as a matrix product rather than as a single value drawn from the definition of the elastic coefficients. This refined stiffness parameter leads to significant improvement of the buckling load, depending on the stacking combination and orientation.
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      Cylindrical Buckling Load of Laminated Columns

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    http://yetl.yabesh.ir/yetl1/handle/yetl/79830
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    contributor authorIzhak Sheinman
    date accessioned2017-05-08T22:24:15Z
    date available2017-05-08T22:24:15Z
    date copyrightMarch 1989
    date issued1989
    identifier other%28asce%290733-9399%281989%29115%3A3%28659%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/79830
    description abstractThe cylindrical buckling load of a composite laminated column is derived from plate theory. The effect of lamina orientation is taken into account by treating the stiffness parameter as a matrix product rather than as a single value drawn from the definition of the elastic coefficients. This refined stiffness parameter leads to significant improvement of the buckling load, depending on the stacking combination and orientation.
    publisherAmerican Society of Civil Engineers
    titleCylindrical Buckling Load of Laminated Columns
    typeJournal Paper
    journal volume115
    journal issue3
    journal titleJournal of Engineering Mechanics
    identifier doi10.1061/(ASCE)0733-9399(1989)115:3(659)
    treeJournal of Engineering Mechanics:;1989:;Volume ( 115 ):;issue: 003
    contenttypeFulltext
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