Aerodynamic design and testing of an axial flow compressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine

Journal of Turbomachinery

Volumn 124, Issue 3, 2002, Pages 331-340

  Wadia, A R ^a   Wolf, D P ^a   Haaser, F G ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; AXIAL FLOW; COMPRESSORS; ELECTRIC POWER GENERATION; VECTORS;

AXIAL FLOW COMPRESSORS; PRESSURE RATIO;

GAS TURBINES;

AERODYNAMICS; AXIAL COMPRESSOR; DESIGN; GAS TURBINE; TESTING;

EID: 0036649005     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1464562     Document Type: Article

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