03 NATURAL GAS COMBUSTION CONTROL COMBUSTION KINETICS EXPERIMENTAL DATA FLAMES KNOCK CONTROL MEDIUM PRESSURE PROPANE TEMPERATURE RANGE 0400-1000 K Gas Turbines Internal Combustion Engines Mathematical Models
A pressure dependent kinetic mechanism for propane oxidation is developed and compared to experimental data from a high pressure flow reactor. Experimental conditions range from 10--15 atm, 650--800 K, and a residence time of 198 ms for propane-air mixtures at an equivalence ratio of 0.4. The experimental results clearly indicate a negative temperature coefficient (NTC) behavior. The chemistry describing this phenomena is critical in understanding automotive engine knock and cool flame oscillations. Results of the numerical model are compared to a spectrum of stable species profiles sampled from the flow reactor. Rate constants and product channels for the reaction of propyl radicals, hydroperoxy-propyl radicals and important isomers (radicals) with O{sub 2} were estimated using thermodynamic properties, with multifrequency quantum Kassel Theory for k(E) coupled with modified strong collision analysis for fall-off. Results of the chemical kinetic model show an NTC region over nearly the same temperature regime as observed in the experiments. Sensitivity analysis identified the key reaction steps that control the rate of oxidation in the NTC region. The model reasonably simulates the profiles for many of the major and minor species observed in the experiments.
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Title
Chemical kinetic modeling of high pressure propane oxidation and comparison to experimental results. Revision 1
Creators
D.N Koert - Wichita State University
W.J Pitz - Lawrence Livermore National Lab., CA (United States)