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Orthogonal Lagrangian Formulation을 이용한 축대칭 형상의 초음속 흡입구 유동 해석 연구
Numerical Simulation for Axisymmetric Supersonic Inlet Using Orthogonal Lagrangian Formulation

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dc.contributor.author이성욱en
dc.contributor.author민대호-
dc.contributor.author김은사-
dc.contributor.author김종암-
dc.creator김종암-
dc.date.accessioned2017-10-23T06:47:20Z-
dc.date.available2017-12-22T09:00:09Z-
dc.date.issued2016-05-26-
dc.identifier.citation한국전산유체공학회 2016년도 춘계학술대회 논문집, pp. 16-17-
dc.identifier.urihttp://hdl.handle.net/10371/135222-
dc.description.sponsorship본 연구는 국방과학연구소의 개발기초 연구사업(0498-20150024)과 민ㆍ군협력 기술사업(Civil-Military Technology Cooperation Program)의 지원을 받아 작성되었습니다.-
dc.language.isoko-
dc.publisher한국전산유체공학회en
dc.subjectOrthogonal Lagrangian Formulation을 이용한 축대칭 형상의 초음속 흡입구 유동 해석 연구en
dc.subject공학en
dc.titleOrthogonal Lagrangian Formulation을 이용한 축대칭 형상의 초음속 흡입구 유동 해석 연구en
dc.title.alternativeNumerical Simulation for Axisymmetric Supersonic Inlet Using Orthogonal Lagrangian Formulation-
dc.typeConference Paper-
dc.contributor.AlternativeAuthorLee, S.-
dc.contributor.AlternativeAuthorMin, D.-
dc.contributor.AlternativeAuthorKim, E.-
dc.contributor.AlternativeAuthorKim, C.-
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dc.description.srndDEPT_NM:기계항공공학부-
dc.description.srndEMAIL:chongam@snu.ac.kr-
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dc.identifier.rimsid175506-
dc.identifier.srnd420160000004648006-
dc.type.rimsCONF-
Appears in Collections:
College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
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