TY - JOUR
T1 - Ignition behavior and surrogate modeling of JP-8 and of camelina and tallow hydrotreated renewable jet fuels at low temperatures
AU - Allen, Casey
AU - Valco, Daniel
AU - Toulson, Elisa
AU - Edwards, Tim
AU - Lee, Tonghun
N1 - Funding Information:
The authors gratefully acknowledge the support of the Defense Logistics Agency (DLA) under Contract SP4701-11-C-0011. Additionally, the authors acknowledge Michigan State University – RTSF – Mass Spectrometry Core for graciously providing access to the GC/MS instrumentation.
PY - 2013/2
Y1 - 2013/2
N2 - The autoignition characteristics of the conventional jet fuel, JP-8, and the alternative jet fuels, camelina and tallow hydrotreated renewable jet (HRJ) fuels, are investigated using a rapid compression machine and the direct test chamber charge preparation approach. Ignition delay measurements are made at low compressed temperatures (625. K. Tc. 730. K), compressed pressures of pc=5, 10, and 20. bar, and equivalence ratios of φ=0.25, 0.5 and 1.0 in air. The HRJ fuels ignite more readily than JP-8 for all tested conditions, consistent with derived cetane number data in the literature. The camelina and tallow HRJ fuels exhibit similar autoignition characteristics, but the two fuels can be distinguished under stoichiometric conditions. Kinetic modeling is conducted with a 2-component surrogate (10% n-dodecane/90% 2-methylundecane) and a single component surrogate (2-methylnonane) to evaluate the potential to predict ignition behavior of the HRJ fuels. Modeling results indicate that the surrogate fuels can only provide useful predictions at a limited set of conditions (pc=5. bar and φ=1.0), and that the agreement of the model and experimental data improves with decreasing compressed pressure. Under most conditions, the 2-component surrogate provides better prediction of ignition behavior, but the single component surrogate is superior at low pressures near the negative temperature coefficient region.
AB - The autoignition characteristics of the conventional jet fuel, JP-8, and the alternative jet fuels, camelina and tallow hydrotreated renewable jet (HRJ) fuels, are investigated using a rapid compression machine and the direct test chamber charge preparation approach. Ignition delay measurements are made at low compressed temperatures (625. K. Tc. 730. K), compressed pressures of pc=5, 10, and 20. bar, and equivalence ratios of φ=0.25, 0.5 and 1.0 in air. The HRJ fuels ignite more readily than JP-8 for all tested conditions, consistent with derived cetane number data in the literature. The camelina and tallow HRJ fuels exhibit similar autoignition characteristics, but the two fuels can be distinguished under stoichiometric conditions. Kinetic modeling is conducted with a 2-component surrogate (10% n-dodecane/90% 2-methylundecane) and a single component surrogate (2-methylnonane) to evaluate the potential to predict ignition behavior of the HRJ fuels. Modeling results indicate that the surrogate fuels can only provide useful predictions at a limited set of conditions (pc=5. bar and φ=1.0), and that the agreement of the model and experimental data improves with decreasing compressed pressure. Under most conditions, the 2-component surrogate provides better prediction of ignition behavior, but the single component surrogate is superior at low pressures near the negative temperature coefficient region.
KW - Autoignition
KW - Hydrotreated renewable jet fuels
KW - JP-8
KW - Rapid compression machine
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U2 - 10.1016/j.combustflame.2012.10.008
DO - 10.1016/j.combustflame.2012.10.008
M3 - Article
AN - SCOPUS:84871920568
SN - 0010-2180
VL - 160
SP - 232
EP - 239
JO - Combustion and Flame
JF - Combustion and Flame
IS - 2
ER -