International Journal of Aeronautical and Space Sciences

  • 제12권4호
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  • Pages.331-345
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  • 2011
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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 Control of a Lifting Surface via Visco-Hysteretic Vibration Absorbers

  • Lacarbonara, Walter (Department of Structural Engineering, SAPIENZA University of Rome) ;
  • Cetraro, Marek (Department of Structural Engineering, SAPIENZA University of Rome)
  • 투고 : 2011.10.10
  • 심사 : 2011.11.29
  • 발행 : 2011.12.30
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초록

In this paper, a visco-hysteretic vibration absorber (VA) is proposed to increase the flutter speed of an airfoil and enhance damping in the pre- and post-flutter regimes. The passive system consists of a parallel arrangement of a dashpot and a rateindependent hysteretic element, represented by the Bouc-Wen differential model. The equations of motion are obtained and various tools of linear and nonlinear dynamics are employed to study the effects of the visco-hysteretic VA in the pre- and postflutter ranges.

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참고문헌

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피인용 문헌

  1. Flutter Control of a Two-Degrees-of-Freedom Airfoil Using a Nonlinear Tuned Vibration Absorber vol.12, pp.5, 2017, https://doi.org/10.1115/1.4036420
  2. A fully passive nonlinear piezoelectric vibration absorber vol.376, pp.2127, 2018, https://doi.org/10.1098/rsta.2017.0142