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A Numerical Study on the Turbulent Schmidt Numbers in a Jet in Crossflow

机译:错流射流中湍流施密特数的数值研究

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摘要

This work presents a numerical study on the turbulent Schmidt numbers in jets in cross-flow. This study contains two main parts. In the first part, the problem of the proper choice of the turbulent Schmidt number in the Reynolds-averaged Navier-Stokes (RANS) jet in crossflow mixing simulations is outlined. The results of RANS employing the shear-stress transport (SST) model of Menter and its curvature correction modification and different turbulent Schmidt number values are validated against experimental data. The dependence of the optimal value of the turbulent Schmidt number on the dynamic RANS model is studied. Furthermore, a comparison is made with the large-eddy simulation (LES) results obtained using the wall-adapted local eddy viscosity (WALE) model. The accuracy given by LES is superior in comparison to RANS results. This leads to the second part of the current study, in which the time-averaged mean and fluctuating velocity and scalar fields from LES are used for the evaluation of the turbulent viscosities, turbulent scalar diffusivities, and the turbulent Schmidt numbers in a jet in crossflow configuration. The values obtained from the LES data are compared with those given by the RANS modeling. The deviations are discussed, and the possible ways for the RANS model improvements are outlined.
机译:这项工作提出了关于横流射流中湍流施密特数的数值研究。这项研究包含两个主要部分。在第一部分中,概述了在横流混合模拟中正确选择雷诺平均Navier-Stokes(RANS)射流中湍流Schmidt数的问题。利用Menter的剪应力传输(SST)模型及其弯曲修正修正和不同的Schmidt湍流数值,对RANS的结果与实验数据进行了验证。研究了湍流施密特数的最优值对动态RANS模型的依赖性。此外,与使用壁适应的局部涡流粘度(WALE)模型获得的大涡流模拟(LES)结果进行了比较。与RANS结果相比,LES提供的精度更高。这导致了本研究的第二部分,其中使用LES的时间平均平均值和脉动速度以及标量场来评估错流射流中的湍流粘度,湍流标量扩散率和湍流Schmidt数组态。从LES数据获得的值与RANS建模给出的值进行比较。讨论了偏差,并概述了用于RANS模型改进的可能方法。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2013年第1期|011505.1-011505.10|共10页
  • 作者单位

    Institute of Combustion Technology, German Aerospace Center (DLR), Stuttgart, 70569 Germany;

    Institute of Combustion Technology, German Aerospace Center (DLR), Stuttgart, 70569 Germany;

    Institute of Combustion Technology, German Aerospace Center (DLR), Stuttgart, 70569 Germany;

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