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A mesh transparent numerical method for large-eddy simulation of compressible turbulent flows

机译:一种用于可压缩湍流大涡模拟的网格透明数值方法

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摘要

A Large Eddy-Simulation code, based on a mesh transparent algorithm, for hybrid unstructured meshes is presented to deal with complex geometries that are often found in engineering flow problems. While tetrahedral elements are very effective in dealing with complex geometry, excessive numerical diffusion often affects results. Thus, prismatic or hexahedral elements are preferable in regions where turbulence structures are important. A second order reconstruction methodology is used since an investigation of a higher order method based upon Lele's compact scheme has shown this to be impractical on general unstructured meshes. The convective fluxes are treated with the Roe scheme that has been modified by introducing a variable scaling to the dissipation matrix to obtain a nearly second order accurate centred scheme in statistically smooth flow, whilst retaining the high resolution TVD behaviour across a shock discontinuity. The code has been parallelised using MPI to ensure portability. The base numerical scheme has been validated for steady flow computations over complex geometries using inviscid and RANS forms of the governing equations. The extension of the numerical scheme to unsteady turbulent flows and the complete LES code have been validated for the interaction of a shock with a laminar mixing layer, a Mach 0.9 turbulent round jet and a fully developed turbulent pipe flow. The mixing layer and round jet computations indicate that, for similar mesh resolution of the shear layer, the present code exhibits results comparable to previously published work using a higher order scheme on a structured mesh. The unstructured meshes have a significantly smaller total number of nodes since tetrahedral elements are used to fill to the far field region. The pipe flow results show that the present code is capable of producing the correct flow features. Finally, the code has been applied to the LES computation of the impingement of a highly under-expanded jet that produces plate shock oscillation. Comparison with other workers' experiments indicates good qualitative agreement for the major features of the flow. However, in this preliminary computation the computed frequency is somewhat lower than that of experimental measurements.
机译:提出了一种基于网格透明算法的大型Eddy模拟代码,用于混合非结构化网格,以处理工程流程问题中经常出现的复杂几何图形。尽管四面体元素在处理复杂的几何形状方面非常有效,但过度的数值扩散通常会影响结果。因此,在湍流结构很重要的区域中,优选棱形或六面体元素。使用二阶重构方法是因为对基于Lele紧致方案的高阶方法的研究表明,这对于一般的非结构化网格是不切实际的。对流通量使用Roe方案进行处理,该方案已通过在耗散矩阵中引入可变比例缩放来修改,以在统计上平滑的流动中获得接近二阶的精确居中方案,同时保留了整个冲击不连续点的高分辨率TVD行为。该代码已使用MPI并行化以确保可移植性。基本数值方案已通过使用无粘性和RANS形式的控制方程进行了复杂几何形状的稳定流计算的验证。已经验证了将数值方案扩展到非恒定湍流和完整的LES代码的作用,以验证冲击与层流混合层,0.9马赫湍流圆形射流以及充分发展的湍流管道之间的相互作用。混合层和圆形射流计算表明,对于剪切层的相似网格分辨率,本代码显示的结果与在结构化网格上使用更高阶方案的先前发布的工作相当。由于使用四面体元素填充到远场区域,因此非结构化网格的节点总数大大减少。管道流量结果表明,当前代码能够产生正确的流量特征。最终,该代码已被应用到LES计算中,该LES计算的是高度膨胀不足的射流的冲击力,该射流会产生板激波振荡。与其他工人实验的比较表明,该流程的主要特征在质量上具有良好的一致性。但是,在此初步计算中,计算出的频率略低于实验测量的频率。

著录项

  • 作者

    Tristanto Indi Himawan;

  • 作者单位
  • 年度 2004
  • 总页数
  • 原文格式 PDF
  • 正文语种 English
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