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...
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 |
Similar Items
-
Modeling of the viscoelastic honeycomb panel equipped with piezoelectric patches in view of vibroacoustic active control design
by: Florens, Corine
Published: (2010) -
Numerical simulation of elastic wave propagation in honeycomb core sandwich plates
by: Tian, Biyu
Published: (2012) -
Dynamic enhancement and multi-axial behavior of honeycombs under combined shear-compression
by: Hou, Bing
Published: (2011) -
Distributed shunted piezoelectric cells for vibroacoustic interface optimization
by: Tateo, Flaviano
Published: (2013) -
Etude de l'impact d'une pointe SNOM sur les propriétés des modes optiques d'une cavité à base de cristaux photoniques
by: Le Gac, Gaëlle
Published: (2009)