Unsteady Flame Embedding (UFE) Subgrid Model for Turbulent Premixed Combustion Simulations
KAUST Grant NumberKUS-11-010-01
Permanent link to this recordhttp://hdl.handle.net/10754/600139
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AbstractWe present a formulation for an unsteady subgrid model for premixed combustion in the flamelet regime. Since chemistry occurs at the unresolvable scales, it is necessary to introduce a subgrid model that accounts for the multi-scale nature of the problem using the information available on the resolved scales. Most of the current models are based on the laminar flamelet concept, and often neglect the unsteady effects. The proposed model's primary objective is to encompass many of the flame/turbulence interactions unsteady features and history effects. In addition it provides a dynamic and accurate approach for computing the subgrid flame propagation velocity. The unsteady flame embedding approach (UFE) treats the flame as an ensemble of locally one-dimensional flames. A set of elemental one dimensional flames is used to describe the turbulent flame structure at the subgrid level. The stretched flame calculations are performed on the stagnation line of a strained flame using the unsteady filtered strain rate computed from the resolved- grid. The flame iso-surface is tracked using an accurate high-order level set formulation to propagate the flame interface at the coarse resolution with minimum numerical diffusion. In this paper the solver and the model components are introduced and used to investigate two unsteady flames with different Lewis numbers in the thin reaction zone regime. The results show that the UFE model captures the unsteady flame-turbulence interactions and the flame propagation speed reasonably well. Higher propagation speed is observed for the lower than unity Lewis number flame because of the impact of differential diffusion.
CitationEl-Asrag H, Nave J-C, Ghoniem A (2010) Unsteady Flame Embedding (UFE) Subgrid Model for Turbulent Premixed Combustion Simulations. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Available: http://dx.doi.org/10.2514/6.2010-201.
SponsorsThis work is supported by the King Abdullah University of Science and Technology (KAUST). Award No. KUS-11-010-01.
Journal48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition