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Critical evaluation of Jet-A spray combustion using propane chemical kinetics in gas turbine combustion simulated by KIVA-IINumerical solutions of the Jet-A spray combustion were obtained by means of the KIVA-II computer code after Jet-A properties were added to the 12 chemical species the program had initially contained. Three different reaction mechanism models are considered. The first model consists of 131 reactions and 45 species; it is evaluated by comparing calculated ignition delay times with available shock tube data, and it is used in the evaluation of the other two simplified models. The simplified mechanisms consider 45 reactions and 27 species and 5 reactions and 12 species, respectively. In the prediction of pollutants NOx and CO, the full mechanism of 131 reactions is considered to be more reliable. The numerical results indicate that the variation of the maximum flame temperature is within 20 percent as compared with that of the full mechanism of 131 reactions. The chemical compositions of major components such as C3H8, H2O, O2, CO2, and N2 are of the same order of magnitude. However, the concentrations of pollutants are quite different.
Document ID
Document Type
Conference Paper
Nguyen, H. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Ying, S.-J.
(South Florida, University Tampa, FL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA PAPER 90-2439
Accession Number
Funding Number(s)
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