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An Approach for Inclusion of a Nonlocal Transition Model in a Parallel Unstructured Computational Fluid Dynamics Code

机译:并行非结构化计算流体力学代码中包含非局部转换模型的方法

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摘要

The implementation of an integral transition model in a parallel unstructured computational fluid dynamics code is described. In particular, an algorithm for gathering the nonlocal boundary layer values (momentum thickness and shape factor) from parallel distributed computational domains is presented. Transition modeling results are presented for a flat plate and for a low pressure turbine, covering a large variation of Reynolds numbers, Mach numbers, turbulence intensities, and incidence angles. Contrary to fully turbulent simulations, transitional predictions are in very good agreement with measurements. Furthermore, the computational overhead of transitional simulations is only 7% for one multigrid cycle.
机译:描述了在并行非结构化计算流体动力学代码中积分过渡模型的实现。特别是,提出了一种用于从并行分布的计算域中收集非局部边界层值(动量厚度和形状因子)的算法。给出了平板和低压涡轮的过渡建模结果,涵盖了雷诺数,马赫数,湍流强度和入射角的较大变化。与完全湍流模拟相反,过渡预测与测量非常吻合。此外,对于一个多网格周期,过渡仿真的计算开销仅为7%。

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  • 来源
    《Journal of turbomachinery》 |2009年第3期|76-82|共7页
  • 作者单位

    Institute of Propulsion Technology, DLR-German Aerospace Center, Cologne D-51147, Germany;

    Aerothermal Methods Group, Rolls-Royce plc., Derby DE24 8BJ, UK;

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