Numerical analysis of the effects of nonuniform surface roughness on compressor stage performance

Journal of Engineering for Gas Turbines and Power

Volumn 133, Issue 7, 2011, Pages

  Morini, Mirko ^a   Pinelli, Michele ^a   Spina, Pier Ruggero ^a   Venturini, Mauro ^a  

^a UNIVERSITY OF FERRARA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

3-D NUMERICAL SIMULATION; AXIAL COMPRESSORS; BASELINE GEOMETRY; BLADE SURFACE; CFD CODES; COMPONENT PERFORMANCE; COMPRESSOR BLADES; COMPRESSOR FOULING; COMPRESSOR PERFORMANCE; COMPRESSOR STAGE; DYNAMIC LEVELS; DYNAMIC PHENOMENA; EXPERIMENTAL DATA; FOULING EFFECTS; GAS TURBINE PERFORMANCE; MICRO-SCALES; NONUNIFORM; NUMERICAL MODELS; PERFORMANCE DETERIORATION; PERFORMANCE MAPS; SINGLE STAGE; STAGE MODELS; STAGE PERFORMANCE; STATOR BLADE; TEST CASE; TURBINE BLADE; TURBINE PERFORMANCE;

CASCADES (FLUID MECHANICS); DETERIORATION; FOULING; GAS TURBINES; METAL ANALYSIS; NASA; NUMERICAL ANALYSIS; ROTORS; STATORS; SURFACE PROPERTIES; SURFACE ROUGHNESS; THREE DIMENSIONAL; THREE DIMENSIONAL COMPUTER GRAPHICS; TURBOMACHINE BLADES;

GAS COMPRESSORS;

EID: 79953233360     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4002350     Document Type: Article

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