Modeling of the viscoelastic honeycomb panel equipped with piezoelectric patches in view of vibroacoustic active control design

Active control has often been considered for low frequency control of noise radiated by trim panels inside aircraft or helicopter cabins. Trim panels are usually made of honeycomb core sandwich because of their high strength to mass ratio. Active control techniques applied to honeycomb panel have no...

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Bibliographic Details
Main Author: Florens, Corine
Language:English
Published: Ecole Centrale Paris 2010
Subjects:
Online Access:http://tel.archives-ouvertes.fr/tel-00545422
http://tel.archives-ouvertes.fr/docs/00/54/54/22/PDF/rapportCFlorens.pdf