Modeling shrouded stator cavity flows in axial-flow compressors

Journal of Turbomachinery

Volumn 122, Issue 1, 2000, Pages 55-61

  Wellborn, S R ^a   Tolchinsky, I ^a   Okiishi, T H ^b  

^a ROLLS ROYCE CORPORATION   (United States)

^b IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CAVITY FLOW; CAVITY MODEL; COMPRESSOR SIMULATION; COMPUTATIONAL ANALYSIS; CORE FLOW; FLOW CHARACTERISTIC; FLOW CONDITION; FLOWTHROUGH; GEOMETRY PARAMETER; HIGHER TEMPERATURES; LABYRINTH SEAL; LEAKAGE FLOW; MASS FLOW; MODEL ESTIMATES; MULTISTAGE COMPRESSOR; ONE-DIMENSIONAL MODEL; OVERALL EFFICIENCY; PRIMARY FLOW; SEAL CLEARANCES; SEAL LEAKAGE; SIGNIFICANT IMPACTS; TEMPERATURE RISE; TWO-COMPONENT;

AXIAL-FLOW COMPRESSORS; STATORS;

SEALS;

AXIAL FLOW COMPRESSOR; CAVITY; FLOW; MATHEMATICAL MODELING;

EID: 0034106609     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.555427     Document Type: Article

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