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    Thermal Dynamic Problems of Reinforced Composite Cylinders

    Source: Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 004::page 941
    Author:
    Victor Birman
    DOI: 10.1115/1.2897665
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Thermal dynamic problems of circular cylindrical composite shells reinforced in the axial and circumferential directions and subject to variations of temperature are considered. Nonlinear governing equations are formulated based on the extension of Donnell shell theory. These equations are used to determine the response of geometrically nonlinear and linear shells to a thermal loading represented by the Heaviside step function (thermal shock). The solution of the nonlinear problem obtained by the assumption that displacements are single-term functions of coordinates is discussed. The analysis of the linear problem illustrates different types of response to thermal shock. The condition of thermally-induced buckling of shells is formulated. Numerical analysis results in conclusions regarding the behavior of shells subject to thermal shock if the temperature is uniformly distributed throughout the shell and stiffeners.
    keyword(s): Composite materials , Cylinders , Shells , Thermal shock , Temperature , Equations , Functions , Numerical analysis AND Buckling ,
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      Thermal Dynamic Problems of Reinforced Composite Cylinders

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    http://yetl.yabesh.ir/yetl1/handle/yetl/106353
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    contributor authorVictor Birman
    date accessioned2017-05-08T23:31:39Z
    date available2017-05-08T23:31:39Z
    date copyrightDecember, 1990
    date issued1990
    identifier issn0021-8936
    identifier otherJAMCAV-26328#941_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106353
    description abstractThermal dynamic problems of circular cylindrical composite shells reinforced in the axial and circumferential directions and subject to variations of temperature are considered. Nonlinear governing equations are formulated based on the extension of Donnell shell theory. These equations are used to determine the response of geometrically nonlinear and linear shells to a thermal loading represented by the Heaviside step function (thermal shock). The solution of the nonlinear problem obtained by the assumption that displacements are single-term functions of coordinates is discussed. The analysis of the linear problem illustrates different types of response to thermal shock. The condition of thermally-induced buckling of shells is formulated. Numerical analysis results in conclusions regarding the behavior of shells subject to thermal shock if the temperature is uniformly distributed throughout the shell and stiffeners.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermal Dynamic Problems of Reinforced Composite Cylinders
    typeJournal Paper
    journal volume57
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2897665
    journal fristpage941
    journal lastpage947
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsCylinders
    keywordsShells
    keywordsThermal shock
    keywordsTemperature
    keywordsEquations
    keywordsFunctions
    keywordsNumerical analysis AND Buckling
    treeJournal of Applied Mechanics:;1990:;volume( 057 ):;issue: 004
    contenttypeFulltext
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