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    Large-Amplitude Vibration Analysis of 3D Braided Composite Cylindrical Shells in an Elastic Medium

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001
    Author:
    Zhi-Min Li
    ,
    Miao Wang
    DOI: 10.1061/(ASCE)AS.1943-5525.0000515
    Publisher: American Society of Civil Engineers
    Abstract: Large-amplitude vibration analysis for a three-dimensional (3D) braided composite cylindrical shell of finite length subjected to static or periodic axial forces has been presented. Based on a new micro-macro-mechanical model, a 3D braided composite may be treated as a cell system, which has been introduced as a representative cell of a 3D braided composite and its components, and the geometry of each cell is deeply dependent on its position in the cross section of the cylindrical shell. The shell is embedded in an elastic medium, which is modeled as a Pasternak elastic foundation. The motion equations are based on a higher-order shear deformation shell theory with a von Kármán-Donnell–type of kinematic nonlinearity. A two-step perturbation technique is used to determine the linear and nonlinear frequency and parametric resonances of the 3D braided cylindrical shells. The numerical illustrations concern the nonlinear vibration behavior of braided composite cylindrical shells with different values of initial stress, of geometric parameter, and of fiber volume fraction.
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      Large-Amplitude Vibration Analysis of 3D Braided Composite Cylindrical Shells in an Elastic Medium

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4244458
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    • Journal of Aerospace Engineering

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    contributor authorZhi-Min Li
    contributor authorMiao Wang
    date accessioned2017-12-30T13:00:36Z
    date available2017-12-30T13:00:36Z
    date issued2016
    identifier other%28ASCE%29AS.1943-5525.0000515.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4244458
    description abstractLarge-amplitude vibration analysis for a three-dimensional (3D) braided composite cylindrical shell of finite length subjected to static or periodic axial forces has been presented. Based on a new micro-macro-mechanical model, a 3D braided composite may be treated as a cell system, which has been introduced as a representative cell of a 3D braided composite and its components, and the geometry of each cell is deeply dependent on its position in the cross section of the cylindrical shell. The shell is embedded in an elastic medium, which is modeled as a Pasternak elastic foundation. The motion equations are based on a higher-order shear deformation shell theory with a von Kármán-Donnell–type of kinematic nonlinearity. A two-step perturbation technique is used to determine the linear and nonlinear frequency and parametric resonances of the 3D braided cylindrical shells. The numerical illustrations concern the nonlinear vibration behavior of braided composite cylindrical shells with different values of initial stress, of geometric parameter, and of fiber volume fraction.
    publisherAmerican Society of Civil Engineers
    titleLarge-Amplitude Vibration Analysis of 3D Braided Composite Cylindrical Shells in an Elastic Medium
    typeJournal Paper
    journal volume29
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000515
    page04015029
    treeJournal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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