Keywords
Natural Gas Combustion, Reduced Mechanisms, Lean Premixed
Abstract
This study has identified useful reduced kinetic schemes that can be used in comprehensive multi-dimensional gas-turbine combustor models. Reduced mechanisms lessen computational cost and possess the capability to accurately predict the overall flame structure, including gas temperatures and key intermediate species such as CH4, CO and NOx. In this study, four-new global mechanisms with 5, 6, 7, and 9 steps based on the full GRI 2.11 mechanism, were developed and evaluated for their potential to model natural-gas chemistry (including NOx chemistry) in gas turbine combustors. These new reduced mechanisms were optimized to model the high pressure and fuel-lean conditions found in gas turbines operating in the lean premixed mode.
Original Publication Citation
Mallampalli, H., T. H. Fletcher, and J. Y. Chen, "Evaluation of CH4/NOx Reduced Mechanisms Used for Modeling Lean Premixed Turbulent Combustion of Natural Gas," Journal of Engineering for Gas Turbines and Power, 120, 703-712 (1998).
BYU ScholarsArchive Citation
Mallampalli, Hemant P.; Fletcher, Thomas H.; and Chen, J Y., "Evaluation of CH4/NOx Reduced Mechanisms Used for Modeling Lean Premixed Turbulent Combustion of Natural Gas" (1998). Faculty Publications. 7055.
https://scholarsarchive.byu.edu/facpub/7055
Document Type
Peer-Reviewed Article
Publication Date
1998
Publisher
ASME
Language
English
College
Ira A. Fulton College of Engineering
Department
Chemical Engineering
Copyright Status
ASME
Copyright Use Information
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