Reduction of unsteady blade loading by beneficial use of vortical and potential disturbances in an axial compressor with rotor clocking

Journal of Turbomachinery

Volumn 120, Issue 4, 1998, Pages 705-713

  Hsu, S T ^a   Wo, A M ^a  

^a NATIONAL TAIWAN UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; POTENTIAL FLOW; ROTORS; STATORS; TURBOMACHINE BLADES; UNSTEADY FLOW; VORTEX FLOW;

AXIAL COMPRESSORS;

COMPRESSORS;

AXIAL COMPRESSOR; BLADE AERODYNAMICS; INSTABILITY; UNSTEADY FLOW; VORTEX;

EID: 0032194603     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841781     Document Type: Article

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