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    Vibration suppression of composite laminated plate with nonlinear energy sink

    Vibration suppression of composite laminated plate with nonlinear energy sink


    Abstract The composite laminated plate is widely used in supersonic aircraft. So, there are many researches about the vibration suppression of composite laminated plate. In this paper, nonlinear energy sink (NES) as an effective method to suppress vibration is studied. The coupled partial differential governing equations of the composite laminated plate with the nonlinear energy sink (NES) are established by using the Hamilton principle. The fourth-order Galerkin discrete method is used to truncate the partial differential equations, which are solved by numerical integration method. Meanwhile study about the precise effectiveness of the nonlinear energy sink (NES) by discussing the different installation location of the nonlinear energy sink (NES) at the same speed. The results indicate that the nonlinear energy sink (NES) can significantly suppress the severe vibration of the composite laminated plate with speed wind loadings in to protect the composite laminated plate from excessive vibration.

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    Titel :

    Vibration suppression of composite laminated plate with nonlinear energy sink

    Beteiligte:
    Zhang, Ye-Wei (Autor:in) / Zhang, Hao (Autor:in) / Hou, Shuai (Autor:in) / Xu, Ke-Fan (Autor:in) / Chen, Li-Qun (Autor:in)
    Erschienen in:

    Acta Astronautica ; 123 ; 109-115

    Erscheinungsdatum :

    2016-02-28

    Format / Umfang :

    7 pages

    ISSN :

    0094-5765

    DOI :

    https://doi.org/10.1016/j.actaastro.2016.02.021

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    Galerkin discrete method , Nonlinear energy sink (NES) , Vibration suppression , Aerodynamic pressure

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