International Journal of Aeronautical and Space Sciences

  • 제7권2호
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  • Pages.70-85
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  • 2006
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Flutter Suppression of Cantilevered Plate Wing using Piezoelectric Materials

  • 발행 : 2006.12.31
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초록

The supersonic flutter suppression of a cantilevered plate wing is studied with the finite element method and the quasi-steady aerodynamic theory. We suppress wing flutter by using piezoelectric materials and electric devices. Two approaches to flutter suppression using piezoelectric materials are presented; an energy-recycling semi-active approach and a negative capacitance approach. To assess their flutter suppression performances, we simulate flutter dynamics of the plate wing to which piezoelectric patches are attached. The critical dynamic pressure drastically increases with our flutter control using a negative capacitor.

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참고문헌

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피인용 문헌

  1. Numerical and Experimental Analysis of the Dynamic Behavior of Piezoelectric Stiffened Composite Plates Subjected to Airflow vol.2019, pp.1563-5147, 2019, https://doi.org/10.1155/2019/2697242