Integrated control of rotating stall and surge in high-speed multistage compression systems

Journal of Turbomachinery

Volumn 120, Issue 3, 1998, Pages 440-445

  Eveker, K M ^a,c   Gysling, D L ^b   Nett, C N ^a   Sharma, O P ^a  

^a PRATT AND WHITNEY   (United States)

^b UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^c INSTITUTE FOR DEFENSE ANALYSES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW TURBOMACHINERY; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; NONLINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); ROTORS; VALVES (MECHANICAL);

HIGH SPEED THREE STAGE AXIAL FLOW COMPRESSORS; ROTATING STALL; SURGE;

COMPRESSORS;

AERODYNAMICS; ROTATING FLOW; STALL;

EID: 0032124662     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841735     Document Type: Article

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