TY - JOUR
T1 - Ignition in nonpremixed counterflowing hydrogen versus heated air
T2 - Computational study with detailed chemistry
AU - Kreutz, T. G.
AU - Law, C. K.
N1 - Funding Information:
The authors are grateful to Mr. C. Fotache, Dr. S. R. Lee, Dr. R. A. Yetter, and Prof. F. L. Dryer of Princeton University for many stimulating conversations, and to Prof. M. D. Smooke of Yale University for the use of his laminar counterftow flame code. We also thank Dr. M. Nishioka of Princeton University for calculating numerous S-curves appearing in Appendix C, to Prof. D. Vlachos of University of Massachusetts at Amherst for performing important supporting computations, and to Dr. G. Balakrishnan for providing his reaction mechanism and associated data. This work was supported by the Army Research Office (DAALO3-90-GO-0220) under the technical monitoring of Dr. D. Mann.
PY - 1996/1
Y1 - 1996/1
N2 - Forced ignition in counterflowing jets of N2-diluted H2 versus heated air has been investigated over a wide range of temperature, pressure, and strain rate by numerical modeling with detailed chemistry and transport. Ignition temperatures calculated at constant strain rates are seen to exhibit a Z-shaped pressure dependence similar to that observed in explosion limits of homogeneous H2/air mixtures. As with the corresponding explosion limits, the first and second ignition limits are governed by the competition for hydrogen radicals between chain branching (H + O2 → O + OH) and termination (H + O2 + M → HO2 + M) pathways, and the third ignition limit involves additional propagation (2HO2 → H2O2 + O2 → 2OH + O2) and branching (HO2 + H2 → H2O2 + H → 2OH + H) pathways that compete with chain termination. Ignition in this inhomogeneous, diffusive system is found to involve a spatially localized ignition 'kernel,' identified as the region near the point of maximum temperature where the rate of hydrogen radical chain branching is maximized. Mass transport of radicals out of the ignition kernel affects the ignition process by competing with chemical reactions within the kernel, particularly in the first and third limits where the dominant ignition chemistry is relatively slow. Ignition temperatures in these limits are found to be much more sensitive to aerodynamic straining than in the second limit. By controlling the width of the ignition kernel and thus the characteristic residence time of key radicals within it, the strain rate is found to determine the dominant chemistry and the relevant ignition limit at any given pressure.
AB - Forced ignition in counterflowing jets of N2-diluted H2 versus heated air has been investigated over a wide range of temperature, pressure, and strain rate by numerical modeling with detailed chemistry and transport. Ignition temperatures calculated at constant strain rates are seen to exhibit a Z-shaped pressure dependence similar to that observed in explosion limits of homogeneous H2/air mixtures. As with the corresponding explosion limits, the first and second ignition limits are governed by the competition for hydrogen radicals between chain branching (H + O2 → O + OH) and termination (H + O2 + M → HO2 + M) pathways, and the third ignition limit involves additional propagation (2HO2 → H2O2 + O2 → 2OH + O2) and branching (HO2 + H2 → H2O2 + H → 2OH + H) pathways that compete with chain termination. Ignition in this inhomogeneous, diffusive system is found to involve a spatially localized ignition 'kernel,' identified as the region near the point of maximum temperature where the rate of hydrogen radical chain branching is maximized. Mass transport of radicals out of the ignition kernel affects the ignition process by competing with chemical reactions within the kernel, particularly in the first and third limits where the dominant ignition chemistry is relatively slow. Ignition temperatures in these limits are found to be much more sensitive to aerodynamic straining than in the second limit. By controlling the width of the ignition kernel and thus the characteristic residence time of key radicals within it, the strain rate is found to determine the dominant chemistry and the relevant ignition limit at any given pressure.
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U2 - 10.1016/0010-2180(95)00121-2
DO - 10.1016/0010-2180(95)00121-2
M3 - Article
AN - SCOPUS:0029657567
SN - 0010-2180
VL - 104
SP - 157
EP - 175
JO - Combustion and Flame
JF - Combustion and Flame
IS - 1-2
ER -