剪切驱动的预混湍流火焰中湍流与标量的相互作用

Haiou Wang, E. Hawkes, H. Kolla, Jacqueline H. Chen
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The alignment characteristics of the flame normal, vorticity, and turbulent strain rate field conditioned on various progress variable iso-surfaces are investigated. Their influence on the scalar gradients and the vorticity production reflecting the turbulence-scalar interactions are examined quantitatively. INTRODUCTION Premixed turbulent combustion is commonly encountered in practical combustion devices such as gas turbines, and spark-ignition engines. An improved understanding of the interactions between turbulence and chemistry is of great importance for turbulent combustion modelling as well as design of clean and efficient combustion devices. In the present paper, turbulenceflame interactions are studied by analysing the coupled dynamics of the scalar gradient, strain rate and vorticity. The directional preference of the scalar gradients with respect to the strain rate is of substantial importance for modelling premixed turbulent combustion. 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摘要

利用模拟时变预混狭缝射流结构中稀薄H2/空气燃烧的DNS数据库,研究了湍流反应流中的湍流-标量相互作用。与以往湍流预混火焰的DNS研究不同,流动中存在平均剪切,并驱动剪切层内小尺度湍流的产生。研究了火焰法向和涡度方向。结果表明,火焰法向优先符合平均流量的最大压缩应变率,涡量优先符合最广泛的平均应变率。前者与火焰锋面有向宽应变率排列的趋势一致,后者与湍流中涡的拉伸有关。研究了火焰法向场、涡度场和湍流应变率场在不同进程变量等面条件下的对准特性。定量地考察了它们对标量梯度和反映湍流-标量相互作用的涡量产生的影响。在实际的燃烧装置中,如燃气轮机和火花点火发动机,通常会遇到预混湍流燃烧。更好地理解湍流与化学之间的相互作用对于湍流燃烧建模以及清洁高效燃烧装置的设计具有重要意义。本文通过分析标量梯度、应变率和涡度的耦合动力学,研究了湍流与火焰的相互作用。标量梯度相对于应变速率的方向偏好对于模拟预混湍流燃烧具有重要意义。具体来说,用- ρNc(niSijnj)表示的所谓的标量-湍流相互作用是过程变量Nc的标量耗散率的输运方程中的源项。在-ρNc (niSijnj)表达式中,ρ为密度,D为扩散系数,ni为火焰法向分量,Sij为应变速率张量,定义为Sij = 0.5(∂ui/∂xj+∂uj/∂xi)。应变速率Sij可以用λ1≥λ2≥λ3约定的主特征值λ1、λ2和λ3来表征,它们由特征方程确定。对应的特征向量分别为e1, e2, e3。火焰法向n用进程变量c定义:
本文章由计算机程序翻译,如有差异,请以英文原文为准。
INTERACTIONS OF TURBULENCE AND SCALARS IN SHEAR-DRIVEN PREMIXED TURBULENT FLAMES USING DNS
The DNS database of modelling lean H2/air combustion in a temporally evolving premixed slot-jet configuration is employed to investigate turbulence-scalar interactions in turbulent reacting flows. In contrast to previous DNS studies of turbulent premixed flames, a mean shear exists in the flow and drives the generation of small-scale turbulence in the shear layer. The orientations of the flame normal and vorticity are examined. It is found that the flame normal preferentially aligns with the most compressive strain rate of the mean flow and the vorticity preferentially aligns with the most extensive mean strain rate. The former is consistent with the fact that the flame front has a tendency to align with the extensive strain rate, while the latter is related to vortex stretching in turbulent flows. The alignment characteristics of the flame normal, vorticity, and turbulent strain rate field conditioned on various progress variable iso-surfaces are investigated. Their influence on the scalar gradients and the vorticity production reflecting the turbulence-scalar interactions are examined quantitatively. INTRODUCTION Premixed turbulent combustion is commonly encountered in practical combustion devices such as gas turbines, and spark-ignition engines. An improved understanding of the interactions between turbulence and chemistry is of great importance for turbulent combustion modelling as well as design of clean and efficient combustion devices. In the present paper, turbulenceflame interactions are studied by analysing the coupled dynamics of the scalar gradient, strain rate and vorticity. The directional preference of the scalar gradients with respect to the strain rate is of substantial importance for modelling premixed turbulent combustion. Specifically, the so-called scalar-turbulence interaction signified by – ρNc(niSijnj) is a source term in the transport equation for the scalar dissipation rate of the progress variable Nc. In the expression signified by –ρNc(niSijnj), ρ is the density, D is the diffusivity, ni is the flame normal component and Sij is the strain rate tensor defined as Sij = 0.5(∂ui/∂xj+∂uj/∂xi). The strain rate Sij can be characterised by the principal eigenvalues λ1, λ2, and λ3 designated by the convention λ1 ≥ λ2 ≥ λ3, which are determined from the characteristic equation. The corresponding eigenvectors are e1, e2 and e3, respectively. The flame normal n is defined in terms of the progress variable c:
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