Response analysis of 6DOF fuselage model during taxiing for comparison of characteristics of single/double stage oleo-pneumatic shock absorber at nose (단-복동형 유.공압 완충장치의 전방장착특성 비교를 위한 6자유도 기체 모형의 지상 이동 응답해석)
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- Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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- 2008.11a
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- pp.734-735
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- 2008