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한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.35 no.4, 2007년, pp.295 - 301
김경석 (한국과학기술원 항공우주공학과 대학원) , 김종윤 (한국과학기술원 항공우주공학과 대학원) , 유재한 (현대기아자동차 연구소) , 배재성 (한국항공대학교 항공우주 및 기계공학부) , 이인 (한국과학기술원 항공우주공학과)
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The aeroelastic characteristics of a wing with control surface freeplay are investigated. The transonic small disturbance equation is used for unsteady aerodynamic forces in subsonic/transonic region. The fictitious mass method is introduced to apply a modal approach to nonlinear structural models. ...
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