Abstract
To characterize the ignition process in homogeneous charge compression ignition engines, high fidelity simulations are performed to study the effects of different initial temperature distributions on the autoignition of a turbulent homogeneous mixture at high pressure. The effects of the initial temperature distribution on the ignition and subsequent heat release are studied by comparison of simulations with three initial random temperature fields having different skewness. It is found that the scalar mixing and turbulence have a significant influence on the initial location and further evolution of the ignition kernels. A comparison of the integrated heat release rates shows that the presence of a hot core leads to early ignition and increased duration of burning, while a cold core leads to a dormant end gas, which is consumed by slow combustion. The extent of flame fronts is quantified by a temperature gradient cut-off, revealing distinct behavior in the appearance of flame fronts for the three cases. Finally, two distinct ignition regimes, namely the spontaneous propagation and the deflagration regimes, are identified, and a predictive criterion is defined based on the spontaneous propagation speed and deflagration speed at the local mixture conditions. The predictions are found to be consistent with the observed results, suggesting a potential strategy in the modeling of HCCI combustion process.
Original language | English |
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Pages (from-to) | 875-882 |
Number of pages | 8 |
Journal | Proceedings of the Combustion Institute |
Volume | 30 |
Issue number | 1 |
DOIs | |
State | Published - 2005 |
Externally published | Yes |
Event | 30th International Symposium on Combustion - Chicago, IL, United States Duration: Jul 25 2004 → Jul 30 2004 |
Funding
The work at UM was supported by the Consortium on HCCI Engine Research directed by the UM and funded by the Department of Energy (DOE), and also by DOE, Office of Basic Energy Sciences, SciDAC Computational Chemistry Program. The work at SNL was supported by the Division of Chemical Sciences, Geosciences and Biosciences, Office of Basic Energy Sciences of the DOE. Calculations were performed at the DOE’s National Energy Research Computational Facility. The authors thank Dr. Scott Mason of Lockheed Martin Corporation for his contribution in the code development, and Drs. John Dec and Magnus Sjöberg of SNL for valuable comments. Appendix A
Funders | Funder number |
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Consortium on HCCI | |
DOE’s National Energy Research Computational Facility | |
Department of Energy | |
U.S. Department of Energy | |
Lockheed Martin Corporation | |
Basic Energy Sciences | |
University of Minnesota | |
Chemical Sciences, Geosciences, and Biosciences Division |
Keywords
- DNS
- HCCI
- Ignition
- Non-uniform temperature
- Reaction front