Optimal Design of Aircraft Gas Turbine System supported by Squeeze Film Damper Using Combined Genetic Algorithm (조합 유전 알고리듬을 이용한 항공기 엔진 시스템의 최적설계)
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- Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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- 2003.05a
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- pp.514-519
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- 2003