Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | SHIN YOU HWAN | - |
| dc.contributor.author | Robin L. Elder | - |
| dc.contributor.author | Lan Bennett | - |
| dc.date.accessioned | 2024-01-13T11:31:23Z | - |
| dc.date.available | 2024-01-13T11:31:23Z | - |
| dc.date.created | 2021-09-29 | - |
| dc.identifier.uri | https://pubs.kist.re.kr/handle/201004/106247 | - |
| dc.language | English | - |
| dc.subject | axial compressor | - |
| dc.subject | boundary layer | - |
| dc.subject | corner separation | - |
| dc.subject | wake band | - |
| dc.title | Boundary layer measurement on the blade surface of a multi-stage axial flow compressor | - |
| dc.type | Conference | - |
| dc.description.journalClass | 1 | - |
| dc.identifier.bibliographicCitation | ASME Turbo Expo 2003, pp.1 - 8 | - |
| dc.citation.title | ASME Turbo Expo 2003 | - |
| dc.citation.startPage | 1 | - |
| dc.citation.endPage | 8 | - |
| dc.citation.conferencePlace | US | - |
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