SHIN YOU HWAN Robin L. Elder Lan Bennett 2024-01-13T11:31:23Z 2024-01-13T11:31:23Z 2021-09-29 https://pubs.kist.re.kr/handle/201004/106247 English axial compressor boundary layer corner separation wake band Boundary layer measurement on the blade surface of a multi-stage axial flow compressor Conference 1 ASME Turbo Expo 2003, pp.1 - 8 ASME Turbo Expo 2003 1 8 US