롤 운동을 고려한 발사체 곡면날개의 플러터 해석 = Flutter analysis of launch vehicle curved fin considering roll motion

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dc.contributor.advisor이인-
dc.contributor.advisorLee, In-
dc.contributor.author백승길-
dc.contributor.authorPaek, Seung-Kil-
dc.date.accessioned2011-12-12T06:59:36Z-
dc.date.available2011-12-12T06:59:36Z-
dc.date.issued1998-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=133594&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26237-
dc.description학위논문(박사) - 한국과학기술원 : 항공우주공학과, 1998.2, [ x, 181 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.subjectRoll spin-
dc.subjectWrap-around fin(WAF)-
dc.subject오일러 방정식-
dc.subject플러터-
dc.subject공력탄성학-
dc.subject롤 회전-
dc.subject곡면 날개-
dc.subjectAeroelasticity-
dc.subjectDelamination buckling-
dc.subjectPost buckling analysis-
dc.subjectBuckling-
dc.subjectComposite laminated panel-
dc.subjectMultiple delaminations-
dc.subjectEuler equations-
dc.subjectFlutter-
dc.title롤 운동을 고려한 발사체 곡면날개의 플러터 해석 = Flutter analysis of launch vehicle curved fin considering roll motion-
dc.typeThesis(Ph.D)-
dc.identifier.CNRN133594/325007-
dc.description.department한국과학기술원 : 항공우주공학과, -
dc.identifier.uid000935174-
dc.contributor.localauthor이인-
dc.contributor.localauthorLee, In-
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AE-Theses_Ph.D.(박사논문)
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