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FEM design of a piezoelectric active control structure. Application to an aircraft wing model

Pommier-Budinger, Valérie and Budinger, Marc and Lever, Phillipe and Richelot, Julien and Bordeneuve-Guibé, Joël FEM design of a piezoelectric active control structure. Application to an aircraft wing model. (2004) In: International Conference on Noise and Vibration Engineering ISMA04, 20-22 Sept 2004, Leuven, Belgique .

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Official URL: http://www.isma-isaac.be/past/conf/isma2004/default_en.phtml


This article shows how a FEM tool can be used to design an active control structure. Two cases of a metalical structure with piezoelectric patches are studied. All the equivalent electromechanical parameters of the structures are calculated with only one modal analysis. A compact model can be deduced and the potentiel of the active structure can be computed.

Item Type:Conference or Workshop Item (Paper)
Audience (conference):International conference proceedings
Uncontrolled Keywords:
Institution:French research institutions > Centre National de la Recherche Scientifique - CNRS (FRANCE)
Other partners > Ecole Nationale Supérieure d’Electronique, Informatique et Radiocommunications de Bordeaux - ENSEIRB (FRANCE)
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE)
Other partners > Université de Bordeaux 1 (FRANCE)
Other partners > Imperial College London (UNITED KINGDOM)
Laboratory name:
Département de Mathématiques, Informatique, Automatique - DMIA (Toulouse, France) - Automatique, Dynamique et Interface des Systèmes - ADIS
Deposited On:15 Jan 2009 13:07

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