Passive Suppression of Nonlinear Panel Flutter Using Piezoceramics with Multi Resonant Circuits

다중 션트회로에 연결된 압전세라믹을 이용한 비선형 패널 플러터의 수동적 억제

  • 문성환 (서울대학교 대학원 항공우주공학과) ;
  • 김승조 (서울대학교 항공우주공학과)
  • Published : 2000.06.22

Abstract

Many analytical and experimental studies on the active suppression of nonlinear panel flutter by using piezoceramic patch have been carried out. However, these active control methods have a few important problems; a large amount of power is required to operate actuators, and additional apparatuses such as sensor systems and controller are needed. In this study passive suppression schemes for nonlinear flutter of composite panel, which is believed to be more robust suppression system than active control in practical operation, are proposed by using piezoelectric inductor-resistor series shunt circuit. Toward the end, a finite element equation of motion for an electromechanically coupled system is proposed using the Hamilton's principle. To achieve the best damping effect, optimal shape and location of the piezoceramic(PZT) patches are determined by using genetic algorithms. The results clearly demonstrate that the passive damping scheme by using piezoelectric shunt circuit can effectively attenuate the flutter.

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