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Development of Boundary Layer on the Blade in an Axial Flow Compressor

Other Titles

축류 압축기 블레이드에서의 경계층 성장

Authors

SHIN, YOU HWAN; Kim, Kwang Ho

Citation

The 3rd National Congress on Fluids Engineering

Keywords

Boundary Layer; Multi-Stage Axial Compressor; Corner Separation; 경계층; 다단 축류 압축기; 모서리 박리

URI

https://pubs.kist.re.kr/handle/201004/105704

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KIST Conference Paper > Others

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