Simulation and Experimental Verification of Typical Aircraft Panel Structure Using Piezoelectric Effect for Vibration and Noise Reduction

Li Zhang; Xia Sheng Sun; Kai Xiang Li

doi:10.4028/www.scientific.net/AMM.387.125

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 387Simulation and Experimental Verification of...

Simulation and Experimental Verification of Typical Aircraft Panel Structure Using Piezoelectric Effect for Vibration and Noise Reduction

Abstract:

A method for the vibration and noise reduction of a typical aircraft panel structure under noise excitations is studied. The noise excitations are caused by travelling wave test device, and the experimental is performed by the piezoelectric switching shunt circuit based on the piezoelectric effect.

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Periodical:

Applied Mechanics and Materials (Volume 387)

Pages:

125-132

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.387.125

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Online since:

August 2013

Authors:

Li Zhang, Xia Sheng Sun, Kai Xiang Li

Keywords:

Experimental Verification, Noise Reduction, Piezoelectric Effect, Simulation, Typical Aircraft Panel Structure, Vibration Reduction

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References

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