Many vibration suppression systems are required to function across a variety of different temperatures, yet most literature ignores the effects of temperature changes on the structure and on the closed loop response. This paper presents an experimental implementation of a vibration suppression system based on a piezoceramic actuator that effectively controls vibration of a clamped panel as it undergoes a variation in ambient temperature. The desire to reduce fatigue in aircraft panels motivates this experimental investigation and implementation.


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    Title :

    Vibration suppression via smart structures across a temperature range


    Contributors:
    Hegewald, T. (author) / Inman, D.J. (author)


    Publication date :

    2001


    Size :

    13 Seiten, 22 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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