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2011•Journal of Engineering ThermophysicsRequires access

Effects of Inlet Boundary Layer on Aerodynamic Performance of a High-Turning Compressor Cascade

Guo Shuang

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Key concepts: Boundary layer suction, Cascade, Inlet, Boundary layer, Suction, Mechanics, Aerodynamics, Flow separation

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Effects of Inlet Boundary Layer on Aerodynamic Performance of a High-Turning Compressor Cascade — Research Paper | ScholarLens