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Computations of Emissions Using a 3-D Combustor ProgramA general 3-D combustor performance program developed by Garrett was extended to predict soot and NOx emissions. The soot formation and oxidation rates were computed by quasi-global models, taking into account the influence of turbulence. Radiation heat transfer was computed by the six-flux radiation mode. The radiation properties include the influence of CO2 and H2O in addition to soot. NOx emissions were computed from a global four-step hydrocarbon oxidation scheme and a set of rate-controlled reactions involving radicals and nitrogen oxides.
Document ID
19830020955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srivatsa, S. K.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Aircraft Propulsion And Power
Accession Number
83N29226
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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