Abstract
This paper investigates the effect of laminar-to-turbulent flame transition modeling on the prediction of cycle-to-cycle variations (CCVs) in large eddy simulation (LES) of spark-ignition (SI) engines. A laminar-to-turbulent flame transition model that describes the non-equilibrium sub-filter flame speed evolution during an early stage of flame kernel growth is developed. In the present model, the flame transition is characterized by the flame kernel size at which the flame transition ends, defined here as the flame transition scale. The proposed model captures the effects that variations in a turbulent flow field have on the evolution of early-stage burning rates, through variations in the flame transition scale. The proposed flame transition model is combined with the front propagation formulation (FPF) method and a spark-ignition model to predict CCVs in a gasoline direct injection SI engine. It is found that multi-cycle LES with the proposed flame transition model reproduces experimentally-observed CCVs satisfactorily. When the transition model is not considered or when variations in the transition process are neglected, CCVs are significantly under-predicted for the case considered here. These results indicate the importance of modeling the laminar-to-turbulent flame transition and the effect of turbulence on the transition process, when predicting CCVs, under certain engine conditions. The LES results are also used to analyze sources for variations in the flame transition. It is found, for the present engine case, that the most important source is the cycle-to-cycle variation in the turbulence dissipation rate, which is used to measure the strength of turbulence in the proposed model, near a spark plug. The large-scale velocity field and the variations of the laminar flame speed due to the mixture composition and thermal stratification are also found to be important factors to contribute to the variations in the flame transition.
Original language | English |
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Pages (from-to) | 2803-2818 |
Number of pages | 16 |
Journal | International Journal of Engine Research |
Volume | 22 |
Issue number | 9 |
DOIs | |
State | Published - Sep 2021 |
Funding
This work used resources at the National Transportation Research Center, a DOE-EERE User Facility at Oak Ridge National Laboratory. The authors thank the Ohio Supercomputer Center (OSC) for the computational resource, Convergent Science for providing the CONVERGE CFD license and the support, and Dr K Dean Edwards for providing the engine geometry file for use in CONVERGE. The preliminary work was presented in the 11th US National Combustion Meeting. The authors thank Professor Paul D Ronney for helpful comments during the meeting. The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by the Department of Energy, Office of Energy Efficiency and Renewable Energy (EERE) and the Department of Defense, Tank and Automotive Research, Development, and Engineering Center (TARDEC), under Award Number DE-EE0007334; and the DOE Office of Energy Efficiency and Renewable Energy (EERE), Vehicle Technologies Office. The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by the Department of Energy, Office of Energy Efficiency and Renewable Energy (EERE) and the Department of Defense, Tank and Automotive Research, Development, and Engineering Center (TARDEC), under Award Number DE-EE0007334; and the DOE Office of Energy Efficiency and Renewable Energy (EERE), Vehicle Technologies Office.
Funders | Funder number |
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DOE-EERE | |
U.S. Department of Defense | |
U.S. Department of Energy | |
Office of Energy Efficiency and Renewable Energy | |
Oak Ridge National Laboratory | |
Tank Automotive Research, Development and Engineering Center | DE-EE0007334 |
Keywords
- Large eddy simulation
- cycle-to-cycle variation
- front propagation formulation method
- internal combustion engine
- laminar-to-turbulent flame transition