Showing results 2 to 6 of 6
Nonlinear aeroelastic analysis of a deployable missile control fin Bae, Jae-Sung; Kim, Dae-Kwan; Shin, Won-Ho; Lee, In; Kim, Seung-Ho, JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.2, pp.264 - 271, 2004-03 |
Nonlinear flutter of aerothermally buckled composite shells with damping treatments Shin, Won-Ho; Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.324, no.3-5, pp.556 - 569, 2009-07 |
Thermal post-buckled behaviors of cylindrical composite shells with viscoelastic damping treatments Shin, Won-Ho; Lee, Seung-Jun; Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.323, no.1-2, pp.93 - 111, 2009-06 |
구조비선형을 고려한 미사일 조종날개의 서보 공탄성 해석 = Aeroservoelastic analysis of missile fin considering structural nonlinearitylink 신원호; Shin, Won-Ho; et al, 한국과학기술원, 2007 |
점탄성 감쇠층이 내삽된 원통형 복합 적층 패널의 동특성 연구 = Dynamic characteristics of cylindrical composite panels with embedded and constrained viscoelastic layerslink 신원호; Shin, Won-Ho; et al, 한국과학기술원, 2002 |
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