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Flutter Suppression of Wing/store Model

날개/스토어 모델의 플러터 억제

  • 배재성 (한국과학기술원 기계공학과(항공우주전공)대학원) ;
  • 김도형 (한국과학기술원 기계공학과(항공우주전공)대학원) ;
  • 양승만 (한국과학기술원 기계공학과(항공우주전공) 대학원) ;
  • 이인 (한국과학기술원 기계공학과(항공우주전공))
  • Published : 2002.07.01

Abstract

Flutter suppression of a wing/store model is investigated. An aircraft wing with a store is modeled as a 2-D typical section. Unsteady aerodynamics of the wing/store model are computed by using doublet hybrid method(DHM) in the freauency-domain, and are approximated by minimumstate(MS) approximation. LQG controller is used to suppress the flutter of the wing/store model and the aeroelastic characteristics of the closed-loop system are investigated. The flutter characteristics of the wing/store model are improved and the flutter speed is increased up to about 24 %.

Keywords

References

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Cited by

  1. Flutter Experiment Equipment Design with Compliant Mechanism vol.22, pp.4, 2012, https://doi.org/10.5050/KSNVE.2012.22.4.393
  2. Flutter Suppression of a Flexible Wing using Sliding Mode Control vol.41, pp.6, 2013, https://doi.org/10.5139/JKSAS.2013.41.6.448