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Modification to Improved Delayed Detached-Eddy Simulation Regarding the Log-Layer Mismatch

机译:对数层不匹配的改进的延迟分离涡流仿真的修改

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摘要

The wall-modeled large-eddy simulation branch of the widely used improved delayed detached-eddy simulation (IDDES) method is supposed to resolve the problems of log-layer mismatch and underprediction of skin friction, as claimed by the authors of the IDDES (Shur, M. L., Spalart, P. R., Strelets, M. K., and Travin, A. K., "A Hybrid RANS-LES Model with Delayed DES and Wall-Modeled LES Capabilities," International Journal of Heat and Fluid Flow, Vol. 29, 2008, pp. 1638-1649). But, some researchers did meet these problems when using the IDDES. Aiming at finding out the reason and seeking a remedy, an analysis of the IDDES is carried out that focuses on the relation between the wall-parallel grid size and the length scale of the energetic turbulent structures at the Reynolds-averaged Navier-Stokes (RANS)/large-eddy simulation (LES) interface, and it reveals that the flaw of the IDDES arises from the fact that, in the IDDES approach, the energetic, large-scale, and stress-carrying turbulent structures in the vicinity of the RANS/LES interface are essentially impossible to well resolve by the LES mode. On the basis of the analysis, a modification to the IDDES is proposed by moving the RANS/LES interface further away from the wall so that, at the RANS/LES interface, the wall-parallel grid size is sufficient to resolve the turbulent structures. The modification is simple in form but has clear physical meaning. Through a series of sensitivity tests, it can be concluded that the modified IDDES does resolve the problems of log-layer mismatch and underprediction of skin friction, and it is applicable to low-, moderate-, and high-Reynolds-number flat plate boundary-layer flows without exception.
机译:如IDDES作者(Shur)所言,广泛使用的改进的延迟分离涡模拟(IDDES)方法的壁模型大涡模拟分支旨在解决对数层不匹配和皮肤摩擦预测不足的问题。 ,ML,Spalart,PR,Strelets,MK和AK,Travin,“具有延迟DES和壁式LES能力的混合RANS-LES模型”,《国际热力和流体流学报》,第29卷,2008年,第2页。 1638-1649)。但是,一些研究人员在使用IDDES时确实遇到了这些问题。为了找出原因并寻求补救措施,对IDDES进行了分析,重点是在雷诺平均Navier-Stokes(RANS)上壁平行网格尺寸与高能湍流结构的长度尺度之间的关系。 )/大涡模拟(LES)界面,它揭示了IDDES的缺陷是由于以下事实引起的:在IDDES方法中,RANS附近的高能,大规模且承载应力的湍流结构LES模式基本上无法很好地解决/ LES接口。在分析的基础上,提出了对IDDES的修改,方法是将RANS / LES界面移离墙壁更远,以便在RANS / LES界面处,平行于墙壁的网格大小足以解决湍流结构。该修饰形式简单,但是具有明确的物理含义。通过一系列的敏感性测试,可以得出结论,改进的IDDES确实解决了对数层不匹配和皮肤摩擦预测不足的问题,并且适用于低,中和高雷诺数平板边界层流量无一例外。

著录项

  • 来源
    《AIAA Journal》 |2020年第2期|712-721|共10页
  • 作者单位

    China Aerodynam Res & Dev Ctr Sci & Technol Scramjet Lab Mianyang 621000 Sichuan Peoples R China;

  • 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
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