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Effects of the Inlet Boundary Layer Thickness on the Rotating Stall in an Axial Compressor
- Title
- Effects of the Inlet Boundary Layer Thickness on the Rotating Stall in an Axial Compressor
- Authors
- 백제현
- Date Issued
- 2008-06-09
- Publisher
- ASME
- Article Type
- Conference
- Citation
- ASME Turbo Expo 2008, 2008-06-09
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