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    Nonlinear Response of Double-Wall Cylindrical Shell Vibrations under Random Excitation

    Source: Journal of Aerospace Engineering:;2006:;Volume ( 019 ):;issue: 001
    Author:
    Vedat Dogan
    ,
    Rimas Vaicaitis
    DOI: 10.1061/(ASCE)0893-1321(2006)19:1(46)
    Publisher: American Society of Civil Engineers
    Abstract: An analytical model is presented to predict the nonlinear response of a double-wall sandwich cylindrical shell system subjected to random excitation. Nonlinear spring-dashpot models are integrated into the system to characterize the behavior of the soft core. Donnell’s thin shell theory is used to develop the governing nonlinear equations of motion. A Monte Carlo simulation of stationary random processes, multimode Galerkin-type approach, and numerical integration procedures are used to develop linear and nonlinear response solutions of simply supported cylindrical shells. Numerical results include time domain response histories, root-mean-square values and response spectral densities. Parametric studies are performed to investigate the effects of nonlinearity, shell thickness, core stiffness, and thickness.
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      Nonlinear Response of Double-Wall Cylindrical Shell Vibrations under Random Excitation

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    contributor authorVedat Dogan
    contributor authorRimas Vaicaitis
    date accessioned2017-05-08T21:16:15Z
    date available2017-05-08T21:16:15Z
    date copyrightJanuary 2006
    date issued2006
    identifier other%28asce%290893-1321%282006%2919%3A1%2846%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45049
    description abstractAn analytical model is presented to predict the nonlinear response of a double-wall sandwich cylindrical shell system subjected to random excitation. Nonlinear spring-dashpot models are integrated into the system to characterize the behavior of the soft core. Donnell’s thin shell theory is used to develop the governing nonlinear equations of motion. A Monte Carlo simulation of stationary random processes, multimode Galerkin-type approach, and numerical integration procedures are used to develop linear and nonlinear response solutions of simply supported cylindrical shells. Numerical results include time domain response histories, root-mean-square values and response spectral densities. Parametric studies are performed to investigate the effects of nonlinearity, shell thickness, core stiffness, and thickness.
    publisherAmerican Society of Civil Engineers
    titleNonlinear Response of Double-Wall Cylindrical Shell Vibrations under Random Excitation
    typeJournal Paper
    journal volume19
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2006)19:1(46)
    treeJournal of Aerospace Engineering:;2006:;Volume ( 019 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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