CFD-based, parametric, design tool for gas turbine combustors from compressor deswirl exit to turbine inlet

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 1, Issue , 2002, Pages 545-552

  Lai, Mark K ^a   Reynolds, Robert S ^a   Armstrong, Jeffrey ^a  

^a HONEYWELL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTOR DESIGNS; CYCLE TIME; TURBINE INLET;

BOUNDARY CONDITIONS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; DESIGN; GAS TURBINES; MATHEMATICAL MODELS;

COMBUSTORS;

EID: 0037000596     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30090     Document Type: Conference Paper

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