Crossflow analogy를 이용한 미사일 동체의 공력 특성 예측A prediction of aerodynamic characteristics for missile body using crossflow analogy

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dc.contributor.advisor박승오-
dc.contributor.advisorPark, Seung-O-
dc.contributor.author이재명-
dc.contributor.authorLee, Jae-Myung-
dc.date.accessioned2011-12-12T07:20:22Z-
dc.date.available2011-12-12T07:20:22Z-
dc.date.issued1999-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=150501&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26838-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1999.2, [ vi, 38 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.subject비례 계수-
dc.subjectSlender Body 이론-
dc.subject횡단면흐름-
dc.subject항력 계수-
dc.subjectDrag coefficient-
dc.subjectProportionality factor-
dc.subjectSlender body theory-
dc.subjectCrossflow-
dc.titleCrossflow analogy를 이용한 미사일 동체의 공력 특성 예측-
dc.title.alternativeA prediction of aerodynamic characteristics for missile body using crossflow analogy-
dc.typeThesis(Master)-
dc.identifier.CNRN150501/325007-
dc.description.department한국과학기술원 : 항공우주공학과, -
dc.identifier.uid000973518-
dc.contributor.localauthor박승오-
dc.contributor.localauthorPark, Seung-O-
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AE-Theses_Master(석사논문)
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