Whirl Flutter Analysis of a 2-DOF Rotor-Nacelle System Using Quasisteady Aerodynamic Theory (준정상 공력이론을 이용한 2자유도계 로터-낫셀 시스템의 훨플러터 해석)
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- Transactions of the Korean Society for Noise and Vibration Engineering
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- v.15 no.7 s.100
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- pp.843-850
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- 2005