Development of hub corner stall and its influence on the performance of axial compressor blade rows

Journal of Turbomachinery

Volumn 121, Issue 1, 1999, Pages 67-77

  Hah, C ^a   Loellbach, J ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; COMPRESSORS; FLOW MEASUREMENT; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; REYNOLDS NUMBER; ROTORS; SUBSONIC FLOW; TRANSONIC FLOW; VORTEX FLOW;

BLADE SUCTION SURFACE; COMPRESSOR STATORS; HUB CORNER STALL;

TURBOMACHINE BLADES;

AXIAL COMPRESSOR; BLADE; MATHEMATICAL ANALYSIS; STALL;

EID: 0032979642     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841235     Document Type: Article

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