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스포일러가 있는 2차원 날개 주위의 비정상 유동 수치 해석 : Numerical analysis of the flowfield around an airfoil with spoiler

DC Field Value Language
dc.contributor.advisor노오현-
dc.contributor.author김지홍-
dc.date.accessioned2010-02-08T04:06:50Z-
dc.date.available2010-02-08T04:06:50Z-
dc.date.copyright1996.-
dc.date.issued1996-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000082759kog
dc.identifier.urihttps://hdl.handle.net/10371/51396-
dc.description학위논문(박사)--서울대학교 대학원 :항공우주공학과,1996.ko
dc.format.extentxi, 153 장ko
dc.language.isokoko
dc.publisher서울대학교 대학원ko
dc.subject정지된 스포일러ko
dc.subjectstationary spoilerko
dc.subject진동하는 스포일러ko
dc.subjectoscillating spoilerko
dc.subject비정상 유동장ko
dc.subjectunsteady flowfiledko
dc.subject변형 동격자ko
dc.subjectflexible dynamic girdko
dc.subject기하학적 보존법칙ko
dc.subjectgeometric conservation lawko
dc.title스포일러가 있는 2차원 날개 주위의 비정상 유동 수치 해석ko
dc.title.alternativeNumerical analysis of the flowfield around an airfoil with spoilerko
dc.typeThesis-
dc.contributor.department항공우주공학과-
dc.description.degreeDoctorko
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