The influence of shrouded stator cavity flows on multistage compressor performance

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1998, Pages

  Wellborn, Steven R ^a   Okiishi, Theodore H ^b  

^a ROLLS ROYCE CORPORATION   (United States)

^b IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL-FLOW COMPRESSORS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; FLOW OF FLUIDS; FLUID MECHANICS; GAS TURBINES;

AERO-DYNAMIC PERFORMANCE; COMPRESSOR PERFORMANCE; MULTISTAGE COMPRESSOR; PERFORMANCE DEGRADATION; PERFORMANCE PENALTIES; SYSTEMATIC CHANGES; TANGENTIAL MOMENTUM; TOTAL-PRESSURE LOSS;

STATORS;

EID: 84971500531     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-012     Document Type: Conference Paper

References (18)

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