TECHNICAL PAPERS: Gas Turbines: Combustion and Fuels

A Critical Evaluation of NOx Modeling in a Model Combustor

[+] Author and Article Information
Lei-Yong Jiang, Ian Campbell

Gas Turbine Environmental Research Center, Institute for Aerospace Research, National Research Council Canada, 1200 Montreal Road, M-10, Ottawa, Ontario, Canada, K1A 0R6

Tel.: 613-993-9235

J. Eng. Gas Turbines Power 127(3), 483-491 (Jun 24, 2005) (9 pages) doi:10.1115/1.1850508 History: Received October 01, 2003; Revised March 01, 2004; Online June 24, 2005
Copyright © 2005 by ASME
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Axial velocity contours and flow path lines
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Axial velocities along the combustor centerline
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Axial velocity profiles at cross sections x=30 mm to 160 mm
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Axial velocity profiles at cross sections x=200 mm to 360 mm
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Upstream temperature contours
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Temperature along the combustor centerline
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Temperature profiles at cross sections x=52 mm to 202 mm
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Temperature profiles at cross sections x=233 mm to 353 mm
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Temperature contours near the flame holder
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Temperature contours near the insulation wall
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No profiles at x=300 mm, PDF combustion model
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Comparison between measured and predicted NO for EDS combustion model
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NO profiles at x=51 mm to 291 mm



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