Active stabilization of axial compressors with circumferential inlet distortion

Journal of Turbomachinery

Volumn 120, Issue 3, 1998, Pages 431-439

  Van Schalkwyk, C M ^a   Paduano, J D ^b   Greitzer, E M ^b   Epstein, A H ^b  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

^b Massachusetts Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; CONTROL SYSTEM ANALYSIS; FEEDBACK CONTROL; INTAKE SYSTEMS; MATHEMATICAL MODELS; SYSTEM STABILITY; TRANSFER FUNCTIONS; UNSTEADY FLOW;

AXIAL COMPRESSORS; CIRCUMFERENTIAL INLET DISTORTION; HYNES-GREITZER DISTORTED FLOW MODEL;

COMPRESSORS;

COMPRESSOR; FLUID FLOW; STABILITY;

EID: 0032124704     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841734     Document Type: Article

References (21)

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