A three-dimensional turbine engine analysis compressor code (TEACC) for steady-state inlet distortion

Journal of Turbomachinery

Volumn 120, Issue 3, 1998, Pages 422-430

  Hale, A ^a   O'Brien W ^b  

^a JACOBS TECHNOLOGY   (United States)

^b Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; EQUATIONS OF MOTION; INTAKE SYSTEMS; ROTORS; TURBOMACHINE BLADES;

INLET DISTORTION; SOFTWARE PACKAGE TURBINE ENGINE ANALYSIS COMPRESSOR CODE (TEACC);

COMPRESSORS;

BLADE; COMPRESSOR; GAS TURBINE;

EID: 0032125008     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841733     Document Type: Article

References (13)

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