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Conference
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dc.contributor.author백제현-
dc.date.accessioned2018-06-18T01:10:08Z-
dc.date.available2018-06-18T01:10:08Z-
dc.date.created2011-04-06-
dc.date.issued2008-06-09-
dc.identifier.urihttps://oasis.postech.ac.kr/handle/2014.oak/58314-
dc.publisherASME-
dc.relation.isPartOfASME Turbo Expo 2008-
dc.relation.isPartOfASME TURBO EXPO 2008-
dc.titleEffects of the Inlet Boundary Layer Thickness on the Rotating Stall in an Axial Compressor-
dc.typeConference-
dc.type.rimsCONF-
dc.identifier.bibliographicCitationASME Turbo Expo 2008-
dc.citation.conferenceDate2008-06-09-
dc.citation.titleASME Turbo Expo 2008-
dc.contributor.affiliatedAuthor백제현-
dc.description.journalClass1-
dc.description.journalClass1-

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