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Adjustment of Subgrid-Scale Parameterizations to Strong Streamline Curvature

机译:将子网格规模的参数化调整为强流线曲率

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摘要

A subgrid-scale model correction for large eddy simulations that address flow fields with embedded areas of poorly resolved strong streamline curvature effects is proposed. The devised modification is termed NaCoo and provides an isotropic correction of the subgrid-scale viscosity based on local centrifugal stability. The degree of stability is identified via a rotational Richardson number that is determined based on non-Galilean-invariant streamline curvature at every grid point. NaCoo allows for a more realistic representation of inadequately resolved coherent turbulent vortices. Its main benefits are 1) conservation of the peak vorticity in the vortex cores, 2) reduction of vortex core radius growth rates, 3) an approach to properties of tangential velocity profiles found in experiments 4) allowance for appropriate turbulence levels in the vicinity of the vortices, and 5) non suppression of vortex core meandering. The derivation of NaCoo, its properties, and sensitivity to numerical and vortex parameters are described in detail. Applications of the correction to single vortices and aircraft wake vortices in a quiescent and turbulent environment demonstrate the capabilities of the pragmatic correction.
机译:提出了针对大涡流模拟的亚网格规模模型校正,该模型解决了具有难以解析的强流线曲率效应的嵌入区域的流场。所设计的改型称为NaCoo,可基于局部离心稳定性提供亚网格规模粘度的各向同性校正。稳定性程度是通过旋转Richardson数确定的,该旋转Richardson数是基于每个栅格点处的非Galile不变流线曲率确定的。 NaCoo可以更真实地表示不充分解决的相干湍流涡流。它的主要好处是:1)保持涡流核心的峰值涡度; 2)减小涡流核心半径的增长率; 3)实验中发现的切向速度分布特性的方法4)允许在附近的湍流水平5)不抑制涡核弯曲。详细介绍了NaCoo的派生,其性质以及对数值和旋涡参数的敏感性。在静态和湍流环境中对单个涡旋和飞机尾流涡旋进行校正的应用证明了务实校正的功能。

著录项

  • 来源
    《AIAA Journal》 |2004年第7期|p.1369-1377|共9页
  • 作者

    Frank Holzaepfel;

  • 作者单位

    DLR, German Aerospace Research Center, Oberpfaffenhofen, 82234 Wessling, Germany;

  • 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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