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    Vibration of Open Cylindrical Shells with Stepped Thickness Variations

    Source: Journal of Engineering Mechanics:;2006:;Volume ( 132 ):;issue: 007
    Author:
    L. Zhang
    ,
    Y. Xiang
    DOI: 10.1061/(ASCE)0733-9399(2006)132:7(780)
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents the first-known exact solutions for vibration of open circular cylindrical shells with multiple stepwise thickness variations based on the Flügge thin shell theory. An open cylindrical shell is assumed to be simply supported along the two straight edges and the remaining two opposite curved edges may have any combination of edge support conditions. The shell is subdivided into segments at the locations of thickness variations. The state-space technique is adopted to derive the homogenous differential equations for a shell segment and the domain decomposition method is employed to impose the equilibrium and compatibility requirements along the interfaces of the shell segments. The correctness of the proposed method is checked against existing results in the open literature and results generated from finite element package ANSYS and excellent agreement is achieved. Several open shells with various combinations of end boundary conditions are studied by the proposed method.
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      Vibration of Open Cylindrical Shells with Stepped Thickness Variations

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    contributor authorL. Zhang
    contributor authorY. Xiang
    date accessioned2017-05-08T22:40:57Z
    date available2017-05-08T22:40:57Z
    date copyrightJuly 2006
    date issued2006
    identifier other%28asce%290733-9399%282006%29132%3A7%28780%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/86281
    description abstractThis paper presents the first-known exact solutions for vibration of open circular cylindrical shells with multiple stepwise thickness variations based on the Flügge thin shell theory. An open cylindrical shell is assumed to be simply supported along the two straight edges and the remaining two opposite curved edges may have any combination of edge support conditions. The shell is subdivided into segments at the locations of thickness variations. The state-space technique is adopted to derive the homogenous differential equations for a shell segment and the domain decomposition method is employed to impose the equilibrium and compatibility requirements along the interfaces of the shell segments. The correctness of the proposed method is checked against existing results in the open literature and results generated from finite element package ANSYS and excellent agreement is achieved. Several open shells with various combinations of end boundary conditions are studied by the proposed method.
    publisherAmerican Society of Civil Engineers
    titleVibration of Open Cylindrical Shells with Stepped Thickness Variations
    typeJournal Paper
    journal volume132
    journal issue7
    journal titleJournal of Engineering Mechanics
    identifier doi10.1061/(ASCE)0733-9399(2006)132:7(780)
    treeJournal of Engineering Mechanics:;2006:;Volume ( 132 ):;issue: 007
    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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