...
首页> 外文期刊>International Journal of Heat and Fluid Flow >Assessment of the SST-IDDES with a shear-layer-adapted subgrid length scale for attached and separated flows
【24h】

Assessment of the SST-IDDES with a shear-layer-adapted subgrid length scale for attached and separated flows

机译:具有用于连接和分离流的剪切层适应的子耕作长度尺度的SST-IDDES

获取原文
获取原文并翻译 | 示例
           

摘要

A shear-layer-adapted subgrid length scale is applied to the improved delayed detached eddy simulation using the shear stress transport background model (SST-IDDES). The aim is to assess the combination of the wall-modeled LES (WMLES) branch of the SST-IDDES with the new length scale in computing attached flows, as well as to assess the effect of the new length scale when it is applied to the SST-IDDES for mitigating the "grey area" issue through initiating a dramatic drop of eddy viscosity in the initial region of a free shear layer. The assessment is conducted through simulations of a turbulent boundary layer, a fully developed channel flow, a near-sonic turbulent jet and a backward-facing step flow. The results provide strong evidence for the conclusion that the SST-IDDES combined with the new length scale performs the same as the original SST-IDDES when its WMLES branch is applied to compute the resolved parts of an attached flow, and the combination helps mitigate the "grey area" issue of the SST-IDDES and accurately represent the K-H instability in the initial region of a free shear layer. In addition, the superiority is particularly remarkable for the simulations with coarse grids.
机译:使用剪切应力运输背景模型(SST-IDDES)将剪切层适配的子级长刻度应用于改进的延迟分离涡流模拟。目的是评估SST-IDDES的壁模拟LES(WMLES)分支的组合在计算的流量中具有新的长度尺度,以及评估新长度尺度的效果应用于应用于SST-IDDES通过在自由剪切层的初始区域中启动涡流的剧烈粘度逐渐减轻“灰色区域”问题。评估通过湍流边界层的模拟,完全开发的通道流,近声音湍流射流和面向后的步长流动进行。结果提供了强有力的证据表明,结合新的长度尺度的SST-IDDE在应用WMLES分支时与原始SST-IDDES相同,以计算所附流量的已分辨率,并且组合有助于减轻措施“灰色区域”问题的SST-IDDES,并准确地表示自由剪切层的初始区域中的KH不稳定性。此外,优于具有粗网格的模拟特别值得注意的。

著录项

  • 来源
    《International Journal of Heat and Fluid Flow》 |2020年第10期|108653.1-108653.14|共14页
  • 作者

    Xiao Maochao; Zhang Yufei;

  • 作者单位

    Tsinghua Univ Sch Aerosp Engn Beijing 100084 Peoples R China|Key Lab Aerodynam Noise Control Mianyang 621000 Sichuan Peoples R China;

    Tsinghua Univ Sch Aerosp Engn Beijing 100084 Peoples R China|Key Lab Aerodynam Noise Control 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
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号