2007
DOI: 10.1016/j.proci.2006.07.086
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Towards large eddy simulation of combustion in spark ignition engines

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Cited by 209 publications
(190 citation statements)
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“…More advanced methods include the artificially thickened flame (ATF/TFM) [9], where the chemical source term is modified to allow the flame to "thicken" and become larger than the mesh size; and the G-equation [10,11], where the flame front is explicitly tracked. All these methods require accurate predictions for the turbulent flame speed, which lead to the development of the Flame Surface Density (FSD) approaches [12,13], the Flame Surface Wrinkling Model [14] and the Coherent Flame Model reformulated for LES [15]. All these methods have common characteristics as they all look for a closure of the turbulent flame speed through the FSD equation and they are restricted to the premixed regime, in most cases away from the broken reaction zones.…”
Section: Introductionmentioning
confidence: 99%
“…More advanced methods include the artificially thickened flame (ATF/TFM) [9], where the chemical source term is modified to allow the flame to "thicken" and become larger than the mesh size; and the G-equation [10,11], where the flame front is explicitly tracked. All these methods require accurate predictions for the turbulent flame speed, which lead to the development of the Flame Surface Density (FSD) approaches [12,13], the Flame Surface Wrinkling Model [14] and the Coherent Flame Model reformulated for LES [15]. All these methods have common characteristics as they all look for a closure of the turbulent flame speed through the FSD equation and they are restricted to the premixed regime, in most cases away from the broken reaction zones.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, Richard et al [27] have proposed the solution of a transport equation for the sub-grid scale flame surface density (i.e., the sgs flame surface per unit volume) to handle nonequilibrium situations in LES of unsteady combustion during spark ignition engine cycles.…”
Section: Introductionmentioning
confidence: 99%
“…All the computations are performed with the AVBP LES code [12,28], which solves the compressible multispecies Navier-Stokes equations. The energy deposition [29] and…”
Section: Numerical Set-upmentioning
confidence: 99%
“…In particular, ICE simulations usually use low order and/or dissipative numerical schemes as well as simple Sub-Grid-Scale (SGS) turbulence models. Concerning numerical schemes, two classes of convective schemes are generally found in the literature: upwind-biased schemes are used by Jhavar and Rutland [8], Dugue et al [9] or Goryntsev et al [10] for instance while the Lax-Wendroff total discretization approach [11] (second order accurate in space and time) is used by Richard et al [12], Vermorel et al [6] or Granet et al [13]. Both of them are known to be very dissipative and a priori not well suited for LES [10].…”
Section: Introductionmentioning
confidence: 99%