Effects of dissipation rate and diffusion rate of the progress variable on local fuel burning rate in premixed turbulent flames

被引:21
|
作者
Savard, Bruno [1 ,2 ]
Blanquart, Guillaume [3 ]
机构
[1] CALTECH, Grad Aerosp Labs, Pasadena, CA 91125 USA
[2] Warsaw Univ Technol, Inst Heat Engn, PL-00665 Warsaw, Poland
[3] CALTECH, Dept Mech Engn, Pasadena, CA 91125 USA
基金
加拿大自然科学与工程研究理事会;
关键词
Turbulent premixed flame; Reaction zone; Flamelet; Dissipation rate; Hydrocarbon fuels; CONDITIONAL MOMENT CLOSURE; LARGE-EDDY SIMULATIONS; HEAT RELEASE RATE; SCALAR DISSIPATION; DIFFERENTIAL DIFFUSION; MEAN REACTION; COMBUSTION; CURVATURE; PROPAGATION; FORMULATION;
D O I
10.1016/j.combustflame.2017.02.025
中图分类号
O414.1 [热力学];
学科分类号
摘要
The validity of the premixed flamelet equations and the dependence of the fuel burning rate on the parameters involved in these equations have been investigated using a large series of direct numerical simulations of turbulent premixed flames in the thin reaction zones (TRZ) and the distributed reaction zones (DRZ) regimes. Methane, toluene, n-heptane, and iso-octane fuels were considered over a wide range of unburnt conditions and turbulence characteristics. Flames with unity and non-unity Lewis numbers were investigated separately to isolate turbulence-chemistry interaction from differential diffusion effects. In both cases, the flamelet equations, which rely on the assumption of a thin reaction zone, are locally valid throughout the TRZ regime, more precisely up to a Karlovitz number at the reaction zone of 10 (based on the definition used in this paper). Consistent with this result, in the unity Lewis number limit, the fuel burning rate is strongly correlated with the dissipation rate of the progress variable, the only parameter in the flamelet equations. In the non-unity Lewis number case, the burning rate is a strong function of both the dissipation rate and the diffusion rate, both of which are parameters in the flamelet equations. In particular, the correlation with these parameters is significantly better than with curvature or tangential strain rate. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:77 / 87
页数:11
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