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Volumn 3, Issue PART B, 2008, Pages 809-822

Modeling of turbulent combustion and radiative heat transfer in a object-oriented cfd code for gas turbine application

Author keywords

[No Author keywords available]

Indexed keywords

AEROENGINES; CFD CODES; COMBUSTION ANALYSIS; COMBUSTION MODEL; COMPUTATIONAL COSTS; CRITICAL ISSUES; DESIGN CONSTRAINTS; DESIGN TECHNIQUE; DEVELOPED MODEL; DIFFUSION FLAME COMBUSTORS; EXHAUST POLLUTANTS; FLAME STABILIZATION; FLAMELET APPROACH; FUNDAMENTAL TOOLS; GAS TURBINE APPLICATIONS; GAS TURBINE DESIGN; GAS TURBINE ENGINE; INDUSTRIAL GAS TURBINES; LINER WALLS; NON-PREMIXED FLAME; OBJECT ORIENTED; OPERATING CONDITION; OPTIMAL TRADEOFFS; PREMIXED; RADIATION MODELS; RADIATIVE HEAT TRANSFER; TEST CASE; TURBULENT COMBUSTION; TURBULENT FLAME;

EID: 69949142513     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-51117     Document Type: Conference Paper
Times cited : (9)

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