NCTAM papers, National Congress of Theoretical and Applied Mechanics, Japan
53rd NCTAM papers, National Congress of Theoretical and Applied Mechanics, Japan
Session ID : 3C1
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OS3
On the Control Efficiency for Flutter Suppression of Composite Plate Wings Using Piezoelectric Sensors/Actuators
*Takehiro Hora
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Abstract
This paper treats an active flutter suppression using piezoelectric sensors/actuators. PVDF sensors are used as modal sensor that identifies specific modes,and PZT actuators are used for flutter suppression. Effect of accuracy of modal sensor output on the control efficiency is discussed through the numerical examples.
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© 2004 Committee for Mechanics and Structure,Science Council
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