Effects of Boundary Layer Suction on Aerodynamic Performance in a High-load Compressor Cascade

Chinese Journal of Aeronautics

Volumn 23, Issue 2, 2010, Pages 179-186

  Shuang, Guo ^a   Shaowen, Chen ^a   Yanping, Song ^a   Yufei, Song ^a   Fu, Chen ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

boundary layer suction; experimental investigation; high load diffusion cascade; turbomachinery

Indexed keywords

AERODYNAMIC PERFORMANCE; BENEFICIAL EFFECTS; BLADE SURFACE; BOUNDARY LAYER SUCTION; CAMBER ANGLE; COMPRESSOR CASCADE; DIFFUSION CASCADE; END-WALL; EXPERIMENTAL INVESTIGATIONS; HIGH-LOAD DIFFUSION CASCADE; LOAD COMPRESSORS; SUCTION FLOW RATE; TOTAL-PRESSURE LOSS; TRAILING EDGES;

AERODYNAMICS; COMPRESSORS; FLOW VISUALIZATION; TURBOMACHINERY;

BOUNDARY LAYERS;

EID: 77951232203     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(09)60202-8     Document Type: Article

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