DSpace at KIST: Development of Boundary Layer on the Blade in an Axial Flow Compressor

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DC Field	Value	Language
dc.contributor.author	SHIN, YOU HWAN	-
dc.contributor.author	Kim, Kwang Ho	-
dc.date.accessioned	2024-01-13T10:31:14Z	-
dc.date.available	2024-01-13T10:31:14Z	-
dc.date.created	2021-09-29	-
dc.identifier.uri	https://pubs.kist.re.kr/handle/201004/105704	-
dc.language	English	-
dc.subject	Boundary Layer	-
dc.subject	Multi-Stage Axial Compressor	-
dc.subject	Corner Separation	-
dc.subject	null	-
dc.subject	null	-
dc.subject	경계층	-
dc.subject	다단 축류 압축기	-
dc.subject	모서리 박리	-
dc.title	Development of Boundary Layer on the Blade in an Axial Flow Compressor	-
dc.title.alternative	축류 압축기 블레이드에서의 경계층 성장	-
dc.type	Conference	-
dc.description.journalClass	2	-
dc.identifier.bibliographicCitation	The 3rd National Congress on Fluids Engineering	-
dc.citation.title	The 3rd National Congress on Fluids Engineering	-
dc.citation.conferencePlace	KO	-

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