유한요소법을 이용한 지능 복합재 구조의 진동 제어 특성 고찰Vibration Control of Smart Composite Structures Using Finite Element Method

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The vibration control characteristics of smart composite structures with piezoelectric material have been inbestigated usinig finite element approach based on the shear deformatiion plate theory. We propose actuation(sensing) effectiveness of each element where piezoelectric material is bonded or embedded. The canti-levered plate with piezoelectric material is solved. It is found that the electrode near the fixed edge has larger actuation effect, and that for the torsional mode the actuation effects are ini phase along the diagonal direction so the electrode pattern along that direction would be more efficient for torsional vibration control.
Publisher
한국항공우주학회
Issue Date
1995-02
Language
Korean
Citation

한국항공우주학회지, v.23, no.1, pp.85 - 96

Citation
Journal of The Korean Society for Aeronautical and Space Sciences, pp.85-96
ISSN
1225-1348
URI
http://hdl.handle.net/10203/8022
Appears in Collection
AE-Journal Papers(저널논문)
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