적응격자 유한요소법을 이용한 스크램제트 입구 유동 해석 = Adaptive grid finite element method for scramjet inlet flow analysis

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dc.contributor.advisor장근식-
dc.contributor.advisorChang, Keun-Shik-
dc.contributor.author이병은-
dc.contributor.authorLee, Byoeng-Eun-
dc.date.accessioned2011-12-12T07:18:15Z-
dc.date.available2011-12-12T07:18:15Z-
dc.date.issued1991-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=67655&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26697-
dc.description학위논문(석사) - 한국과학기술원 : 항공공학과, 1991.2, [ [v], 53 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.title적응격자 유한요소법을 이용한 스크램제트 입구 유동 해석 = Adaptive grid finite element method for scramjet inlet flow analysis-
dc.typeThesis(Master)-
dc.identifier.CNRN67655/325007-
dc.description.department한국과학기술원 : 항공공학과, -
dc.identifier.uid000891338-
dc.contributor.localauthor장근식-
dc.contributor.localauthorChang, Keun-Shik-
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AE-Theses_Master(석사논문)
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