On the development and application of the fast-response aerodynamic probe system in Turbomachines - Part 2: Flow, surge, and stall in a centrifugal compressor

Journal of Turbomachinery

Volumn 122, Issue 3, 2000, Pages 517-526

  Roduner, C ^a   Kupferschmied, P ^a   Koppel, P ^a   Gyarmathy, G ^a  

^a ETH ZURICH   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

DIFFUSERS (FLUID); FLOW MEASUREMENT; PRESSURE MEASUREMENT; PROBES; ROTORS; SENSORS; SUBSONIC AERODYNAMICS; SURGES (FLUID); TURBOMACHINE BLADES; TURBULENT FLOW; UNSTEADY FLOW;

CENTRIFUGAL COMPRESSOR; FAST RESPONSE AERODYNAMIC PROBE SYSTEM; MILD SURGE; PRESSURE SENSOR; ROTATING STALL;

COMPRESSORS;

AERODYNAMIC PROBE; CENTRIFUGAL COMPRESSOR; FLOW MEASUREMENT; MEASURING INSTRUMENT; STALL; SURGE;

EID: 0034233230     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1303827     Document Type: Conference Paper

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