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    Buckling and Post-buckling of Composite Plates and Shells Subjected to Elevated Temperature

    Source: Journal of Applied Mechanics:;1993:;volume( 060 ):;issue: 002::page 514
    Author:
    V. Birman
    ,
    C. W. Bert
    DOI: 10.1115/1.2900823
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Effects of temperature on buckling and post-buckling behavior of reinforced and unstiffened composite plates or cylindrical shells are considered. First, equilibrium equations are formulated for a shell subjected to the simultaneous action of a thermal field and an axial loading. These equations are used to predict a general form of the algebraic equations describing the post-buckling response of a shell. Conditions for the snap-through of a shell subjected to thermomechanical loading are formulated. As an example, the theory is applied to prediction of post-buckling response of flat large-aspect-ratio panels reinforced in the direction of their short edges.
    keyword(s): Temperature , Composite materials , Plates (structures) , Buckling , Shells , Equations , Equilibrium (Physics) , Temperature effects AND Pipes ,
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      Buckling and Post-buckling of Composite Plates and Shells Subjected to Elevated Temperature

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111462
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    • Journal of Applied Mechanics

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    contributor authorV. Birman
    contributor authorC. W. Bert
    date accessioned2017-05-08T23:40:32Z
    date available2017-05-08T23:40:32Z
    date copyrightJune, 1993
    date issued1993
    identifier issn0021-8936
    identifier otherJAMCAV-26349#514_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111462
    description abstractEffects of temperature on buckling and post-buckling behavior of reinforced and unstiffened composite plates or cylindrical shells are considered. First, equilibrium equations are formulated for a shell subjected to the simultaneous action of a thermal field and an axial loading. These equations are used to predict a general form of the algebraic equations describing the post-buckling response of a shell. Conditions for the snap-through of a shell subjected to thermomechanical loading are formulated. As an example, the theory is applied to prediction of post-buckling response of flat large-aspect-ratio panels reinforced in the direction of their short edges.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBuckling and Post-buckling of Composite Plates and Shells Subjected to Elevated Temperature
    typeJournal Paper
    journal volume60
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2900823
    journal fristpage514
    journal lastpage519
    identifier eissn1528-9036
    keywordsTemperature
    keywordsComposite materials
    keywordsPlates (structures)
    keywordsBuckling
    keywordsShells
    keywordsEquations
    keywordsEquilibrium (Physics)
    keywordsTemperature effects AND Pipes
    treeJournal of Applied Mechanics:;1993:;volume( 060 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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