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Boundary layer measurement on the blade surface of a multi-stage axial flow compressor

Authors

SHIN YOU HWAN; Robin L. Elder; Lan Bennett

Citation

ASME Turbo Expo 2003, pp.1 - 8

Keywords

axial compressor; boundary layer; corner separation; wake band

URI

https://pubs.kist.re.kr/handle/201004/106247

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KIST Conference Paper > Others

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