Rotating stall control in a high-speed stage with inlet distortion: Part I—radial distortion

Journal of Turbomachinery

Volumn 121, Issue 3, 1999, Pages 510-516

  Spakovszky, Z S ^a   Weigl, H J ^a   Pacluano, J D ^a   Van Schalkwyk, C M ^b   Suder, K L ^c   Bright, M M ^c  

^a Massachusetts Institute of Technology   (United States)

^b SCIENTIFIC SYSTEMS COMPANY INC   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; FEEDBACK CONTROL; FLOW CONTROL; INTAKE SYSTEMS; MASS TRANSFER; RADIAL FLOW; ROTATIONAL FLOW; STEADY FLOW; TRANSFER FUNCTIONS; TRANSONIC FLOW;

INLET DISTORTION; ROTATING STALL CONTROL; SINGLE-INPUT SINGLE-OUTPUT (SISO) CONTROL;

AXIAL FLOW TURBOMACHINERY;

AXIAL FLOW COMPRESSOR; CONTROL METHOD; FLOW; INLET; STALL;

EID: 0032703439     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841345     Document Type: Article

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