Comparative study on vibration control methodologies applied to adaptive thin-walled anisotropic cantilevers (Q2565721)

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Comparative study on vibration control methodologies applied to adaptive thin-walled anisotropic cantilevers
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    Comparative study on vibration control methodologies applied to adaptive thin-walled anisotropic cantilevers (English)
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    28 September 2005
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    aircraft wing
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    piezoelectric effect
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    closed-loop dynamic response
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