Effect of upstream rotor vortical disturbances on the time-averaged performance of axial compressor stators: Part 2—rotor tip vortex/streamwise vortex-stator blade interactions

Journal of Turbomachinery

Volumn 121, Issue 3, 1999, Pages 387-397

  Valkov, T V ^a   Tan, C S ^b  

^a Shell International Limited   (United Kingdom)

^b Massachusetts Institute of Technology Cambridge   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; COMPRESSORS; COMPUTER SIMULATION; FLOW INTERACTIONS; LEAKAGE (FLUID); ROTORS; UNSTEADY FLOW; VORTEX FLOW; WAKES;

COMPRESSOR STATORS; ENERGY RECOVERY; MIXED-OUT STEADY FLOW APPROXIMATION;

TURBOMACHINE BLADES;

AXIAL COMPRESSOR; INTERACTION; ROTOR; STATOR; VORTEX;

EID: 0032723963     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841331     Document Type: Article

References (11)

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