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Large-Eddy Simulation/Reynolds-Averaged Navier-Stokes Simulations of High-Speed Mixing Processes

机译:高速混合过程的大涡模拟/雷诺平均Navier-Stokes模拟

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摘要

A large-eddy simulation/Reynolds-averaged Navier-Stokes model is applied to three high-speed mixing layers and three sonic injection flows to generate data suitable for evaluating two current Reynolds-averaged Navier-Stokes models for turbulent mass diffusivity. These models solve transport equations for concentration variance and dissipation rate and differ in the constitutive relation for the turbulent mass diffusivity and the form of the evolution equation for the dissipation rate. The predictive capability of the large-eddy simulation/Reynolds-averaged Navier-Stokes model is assessed through simulations of an air-air mixing-layer experiment and a sonic ethylene injection into a Mach 2.0 airstream. This model provides good predictions of the mean velocity, turbulence intensity, and rms temperature fluctuation throughout the shear layer flowfield but slightly over-predicts the spreading rate of the mixing layer. The simulation of the sonic injection is in generally good agreement with the experiment but underpredicts the level of jet entrainment. Four other large-eddy simulation/Reynolds-averaged Navier-Stokes data sets, involving the replacement of the lower airstream in the mixing-layer configuration by an argon stream and a helium stream, and a replacement of the injectant gas in the sonic injection experiment with argon and helium are also generated. All data sets are "mined" to extract turbulent mass diffusivities, concentration variances, and scalar dissipation rates associated with the resolved eddy motion. The results show that both models can be optimized to achieve a good match with the exact scalar variance production rate.
机译:将大涡模拟/雷诺平均Navier-Stokes模型应用于三个高速混合层和三个声波注入流,以生成适合评估两个当前雷诺平均Navier-Stokes模型湍流质量扩散率的数据。这些模型求解浓度变化和耗散率的输运方程,湍流质量扩散率的本构关系不同,耗散率的演化方程形式也不同。大涡模拟/雷诺平均Navier-Stokes模型的预测能力是通过模拟空气-空气混合层实验和向2.0马赫数的气流中注入乙烯进行评估的。该模型可以很好地预测整个剪切层流场中的平均速度,湍流强度和均方根温度波动,但会稍微高估混合层的扩展速率。声波注入的模拟通常与实验吻合得很好,但是低估了射流夹带的水平。其他四个大涡模拟/雷诺平均Navier-Stokes数据集,包括用氩流和氦流替换混合层结构中的下部气流,以及在声波注入实验中替换注入气体也会产生氩气和氦气“挖掘”所有数据集以提取与解析的涡旋运动相关的湍流质量扩散率,浓度方差和标量耗散率。结果表明,可以对这两个模型进行优化,以使其与精确的标量方差产生率完全匹配。

著录项

  • 来源
    《AIAA Journal》 |2014年第7期|1486-1501|共16页
  • 作者单位

    North Carolina State University, Raleigh, North Carolina 27695;

    North Carolina State University, Raleigh, North Carolina 27695;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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