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LARGE EDDY SIMULATION OF REARWARE-FACING STEP FLOW

机译:面向反应的逐步流动的大涡模拟

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摘要

In conventiona large eddy simulation(LES) models, the filtered Navier-Stokes equations(NSE) are supplemented by subgrid-scale(SGS) models that emulate the energy transfer from large scales toward the subgrid scales, where it will eventually be dissipated by molecular viscosity. An alternative approach involves solving the unfiltered NSE using high-resolution monotone algorithms for which implicit SGS models are provided by the intrinsic nonlinear high-frequency filters built into the convection discretization . This monotonically integrated LES(MILES) model is to be distinguished from underresolved direct numerical simulation models relying on other numerical methods(not necessarily monotonic) to represent the required damping, which will not necessarily ensure the correct distribution of energy among the large scales. Results from LES and MILES of turbulent rearward-facing step flows suggest that LES is independent of the details of the SGS model if it can adequately channel kinetic energy out of eddies close to the cutoff wave number to prevent aliasing , provided that the resolution is fine enough to ensure that the cutoff wave number is within the inertial subrange. Comparison with experimental data indicates good agreement for global quantities and first- and second-order statistical moments of velocity. Based on the simulations and the comparison with experimental data, the behavior of the flow in the free shear layer and in the reattachment region is presented together with a discussion of flow separation and reattachment.
机译:在传统的大涡模拟(LES)模型中,过滤后的Navier-Stokes方程(NSE)由子网格规模(SGS)模型补充,该模型模拟了从大尺度向子网格尺度的能量转移,在该过程中,能量最终会被分子消散粘度。另一种方法是使用高分辨率单调算法求解未滤波的NSE,对流离散化中内置的固有非线性高频滤波器为其提供了隐式SGS模型。这种单调集成的LES(MILES)模型与依赖于其他数值方法(不一定是单调)来表示所需阻尼的欠解析直接数值模拟模型有所区别,这不一定能确保大范围能量的正确分配。 LES和MILES的湍流后向步进流的结果表明,如果LES能够将动能从接近截止波数的涡流中充分导引出来以防止混叠,则LES与SGS模型的细节无关,只要分辨率很好即可。足以确保截止波数在惯性子范围内。与实验数据的比较表明,总体数量以及速度的一阶和二阶统计矩具有良好的一致性。在模拟的基础上,并与实验数据进行比较,介绍了自由剪切层和再附着区域中的流动行为,并对流动分离和再附着进行了讨论。

著录项

  • 来源
    《AIAA Journal》 |1999年第11期|p.1401-1410|共10页
  • 作者

    C.FUREBY;

  • 作者单位
  • 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 航空、航天;航空;
  • 关键词

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