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    Nonlinear Vibration of Composite Shell Subjected to Resonant Excitations

    Source: Journal of Aerospace Engineering:;2000:;Volume ( 013 ):;issue: 002
    Author:
    Jamal F. Nayfeh
    ,
    Nicholas J. Rivieccio
    DOI: 10.1061/(ASCE)0893-1321(2000)13:2(59)
    Publisher: American Society of Civil Engineers
    Abstract: Analysis of the vibration of a shallow, simply supported, nonsymmetric unbalanced cross-ply laminated, circular cylindrical composite shell is presented. The subject is particularly relevant, considering the widespread use of cylindrical shell structures in engineering applications. This research applies the discretized Lagrangian/method of multiple scales solution technique. The Donnell shallow shell strain-displacement relations and the single-mode displacement field from the linear eigenvalue problem are applied. The system Lagrangian is developed and integrated over the spatial domain and then substituted into Lagrange's equation. The resulting equation of motion is a second-order temporally nonlinear ordinary differential equation in the form of the Duffing oscillator. The natural frequency, the coefficient of the cubic nonlinearity, and the strength of the nonlinearity are investigated. The method of multiple scales is applied to the nonlinear equation of motion in order to analyze the frequency response. Primary resonance, subharmonic resonance, and superharmonic resonance are analyzed.
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      Nonlinear Vibration of Composite Shell Subjected to Resonant Excitations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44919
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    contributor authorJamal F. Nayfeh
    contributor authorNicholas J. Rivieccio
    date accessioned2017-05-08T21:16:01Z
    date available2017-05-08T21:16:01Z
    date copyrightApril 2000
    date issued2000
    identifier other%28asce%290893-1321%282000%2913%3A2%2859%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44919
    description abstractAnalysis of the vibration of a shallow, simply supported, nonsymmetric unbalanced cross-ply laminated, circular cylindrical composite shell is presented. The subject is particularly relevant, considering the widespread use of cylindrical shell structures in engineering applications. This research applies the discretized Lagrangian/method of multiple scales solution technique. The Donnell shallow shell strain-displacement relations and the single-mode displacement field from the linear eigenvalue problem are applied. The system Lagrangian is developed and integrated over the spatial domain and then substituted into Lagrange's equation. The resulting equation of motion is a second-order temporally nonlinear ordinary differential equation in the form of the Duffing oscillator. The natural frequency, the coefficient of the cubic nonlinearity, and the strength of the nonlinearity are investigated. The method of multiple scales is applied to the nonlinear equation of motion in order to analyze the frequency response. Primary resonance, subharmonic resonance, and superharmonic resonance are analyzed.
    publisherAmerican Society of Civil Engineers
    titleNonlinear Vibration of Composite Shell Subjected to Resonant Excitations
    typeJournal Paper
    journal volume13
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2000)13:2(59)
    treeJournal of Aerospace Engineering:;2000:;Volume ( 013 ):;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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