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    Bending Instability of Composite Tubes

    Source: Journal of Aerospace Engineering:;1996:;Volume ( 009 ):;issue: 002
    Author:
    Long-yuan Li
    DOI: 10.1061/(ASCE)0893-1321(1996)9:2(58)
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a set of simple formulations is derived to predict the instability critical loads of orthotropic composite tubes under pure bending. The formulations are based on the assumption that the instability of an orthotropic composite tube under pure bending is due to the ovalization of its cross section. For the static instability case, the ovalization increases steadily as the curvature increases, which results in a reduction in the bending rigidity of the tube. The interaction of longitudinal bending and cross-section ovalization causes the tube to have a limit load instability. For the dynamic instability case, the instability of the tube is due to the interaction of two vibrations, one is the longitudinal bending of the tube as a beam, the other is the circumferential bending of the tube as a thin-walled shell.
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      Bending Instability of Composite Tubes

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    contributor authorLong-yuan Li
    date accessioned2017-05-08T21:15:52Z
    date available2017-05-08T21:15:52Z
    date copyrightApril 1996
    date issued1996
    identifier other%28asce%290893-1321%281996%299%3A2%2858%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44829
    description abstractIn this paper, a set of simple formulations is derived to predict the instability critical loads of orthotropic composite tubes under pure bending. The formulations are based on the assumption that the instability of an orthotropic composite tube under pure bending is due to the ovalization of its cross section. For the static instability case, the ovalization increases steadily as the curvature increases, which results in a reduction in the bending rigidity of the tube. The interaction of longitudinal bending and cross-section ovalization causes the tube to have a limit load instability. For the dynamic instability case, the instability of the tube is due to the interaction of two vibrations, one is the longitudinal bending of the tube as a beam, the other is the circumferential bending of the tube as a thin-walled shell.
    publisherAmerican Society of Civil Engineers
    titleBending Instability of Composite Tubes
    typeJournal Paper
    journal volume9
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1996)9:2(58)
    treeJournal of Aerospace Engineering:;1996:;Volume ( 009 ):;issue: 002
    contenttypeFulltext
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