동적강성을 갖는 비행체 조종날개의 플러터 해석 = Flutter analysis of a flight vehicle control wing with dynamic stiffness

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dc.contributor.advisor이인-
dc.contributor.advisorLee, In-
dc.contributor.author백승길-
dc.contributor.authorPaek, Seung-Kil-
dc.date.accessioned2011-12-12T07:18:30Z-
dc.date.available2011-12-12T07:18:30Z-
dc.date.issued1993-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=68512&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26714-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1993.2, [ vii, 54 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.title동적강성을 갖는 비행체 조종날개의 플러터 해석 = Flutter analysis of a flight vehicle control wing with dynamic stiffness-
dc.typeThesis(Master)-
dc.identifier.CNRN68512/325007-
dc.description.department한국과학기술원 : 항공우주공학과, -
dc.identifier.uid000911294-
dc.contributor.localauthor이인-
dc.contributor.localauthorLee, In-
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AE-Theses_Master(석사논문)
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