TY - JOUR
T1 - A high-pressure rapid compression machine study of n-propylbenzene ignition
AU - Darcy, D.
AU - Nakamura, H.
AU - Tobin, C. J.
AU - Mehl, M.
AU - Metcalfe, W. K.
AU - Pitz, W. J.
AU - Westbrook, C. K.
AU - Curran, H. J.
N1 - Funding Information:
NUIG acknowledge the financial support of the Saudi Arabian Oil Company. The LLNL work was performed under the auspices of the US Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344 and was supported by the US Department of Energy, Office of Vehicle Technologies (program manager Gurpreet Singh). Co-author H.N. acknowledges the financial support “Young Researcher Overseas Visits Program for Vitalizing Brain Circulation” from Japan Society of the Promotion for Science.
PY - 2014/1/1
Y1 - 2014/1/1
N2 - This study presents new ignition delay data measured in a rapid compression machine over a wide range temperature, pressure and fuel/air ratio. This data is an extension of that measured previously (D. Darcy, C.J. Tobin, K. Yasunaga, J.M. Simmie, J. Würmel, T. Niass, O. Mathieu, S.S. Ahmed, C.K. Westbrook, H.J. Curran, Combust. Flame, 159 (2012) 2219-2232.) for the oxidation of n-propylbenzene in a high-pressure shock tube. The data was obtained for equivalence ratios of 0.29, 0.48, 0.96, and 1.92, at compressed gas pressures of 10, 30 and 50. atm, and over the temperature range of 650-1000. K. Experimental data was also obtained at 50. atm for all equivalence ratios in our new heated high-pressure shock tube and this is also presented here. Comparisons between the data obtained in both the rapid compression machine and the shock tube facilities showed excellent agreement. A previously published chemical kinetic mechanism has been improved and a low-temperature reaction mechanism has been added to simulate ignition delay times at the lower temperature conditions of this study by adding the appropriate species and reactions including alkyl-peroxyl and hydroperoxy-alkyl radical chemistry. Special attention was given to RȮ2 isomerizations and HȮ2 elimination reactions involving the secondary benzylic site on n-propylbenzene to obtain good agreement with the present experimental results. In general, good agreement was obtained between the model and experiments and consistent trends were observed and these are discussed.
AB - This study presents new ignition delay data measured in a rapid compression machine over a wide range temperature, pressure and fuel/air ratio. This data is an extension of that measured previously (D. Darcy, C.J. Tobin, K. Yasunaga, J.M. Simmie, J. Würmel, T. Niass, O. Mathieu, S.S. Ahmed, C.K. Westbrook, H.J. Curran, Combust. Flame, 159 (2012) 2219-2232.) for the oxidation of n-propylbenzene in a high-pressure shock tube. The data was obtained for equivalence ratios of 0.29, 0.48, 0.96, and 1.92, at compressed gas pressures of 10, 30 and 50. atm, and over the temperature range of 650-1000. K. Experimental data was also obtained at 50. atm for all equivalence ratios in our new heated high-pressure shock tube and this is also presented here. Comparisons between the data obtained in both the rapid compression machine and the shock tube facilities showed excellent agreement. A previously published chemical kinetic mechanism has been improved and a low-temperature reaction mechanism has been added to simulate ignition delay times at the lower temperature conditions of this study by adding the appropriate species and reactions including alkyl-peroxyl and hydroperoxy-alkyl radical chemistry. Special attention was given to RȮ2 isomerizations and HȮ2 elimination reactions involving the secondary benzylic site on n-propylbenzene to obtain good agreement with the present experimental results. In general, good agreement was obtained between the model and experiments and consistent trends were observed and these are discussed.
KW - Butylbenzene
KW - Ignition
KW - Ignition delay times
KW - Propylbenzene
KW - Rapid compression machine
KW - Shock tube
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U2 - 10.1016/j.combustflame.2013.08.001
DO - 10.1016/j.combustflame.2013.08.001
M3 - Article
AN - SCOPUS:84887820774
SN - 0010-2180
VL - 161
SP - 65
EP - 74
JO - Combustion and Flame
JF - Combustion and Flame
IS - 1
ER -