AbstractThe Bachalo-Johnson experiment on an axisymmetric bump has been a primary validation case for turbulence'/> Large-Eddy and Direct Numerical Simulations of the Bachalo-Johnson Flow with Shock-Induced Separation
首页> 外文期刊>Flow, turbulence and combustion >Large-Eddy and Direct Numerical Simulations of the Bachalo-Johnson Flow with Shock-Induced Separation
【24h】

Large-Eddy and Direct Numerical Simulations of the Bachalo-Johnson Flow with Shock-Induced Separation

机译:Bachalo-Johnson流量的大涡流和直接数值模拟,具有冲击诱导的分离

获取原文
获取原文并翻译 | 示例
           

摘要

AbstractThe Bachalo-Johnson experiment on an axisymmetric bump has been a primary validation case for turbulence models in shock-boundary-layer interactions since the 1980’s. In the present work, Wall-Modelled Large-Eddy Simulations (WMLES) of this flow were conducted using Improved Delayed Detached-Eddy Simulation (IDDES) as the sub-grid-scale (SGS) and wall model, with a synthetic turbulence generator, expecting close enough agreement with experiment. However, the WMLES results are disappointing, even in terms of the shock position, even though the results from two grids with 4.7 × 108and 1.6 × 109cells respectively agree well with each other. This failure of grid refinement to warn of an inaccurate simulation is of great concern, and the reasons for it are explored. We then conducted a Direct Numerical Simulation (DNS) embedded in the LES over a reduced domain, with 8 × 109grid cells. The DNS has a far more accurate shock position and overall pressure distribution. The skin friction in the favourable pressure gradient is also much higher than in the LES; thus, wide differences appear upstream of the shock wave, most probably caused by the rapid acceleration which leads to atypical shear-stress profiles. Other SGS models were tried, and performed worse than IDDES. The DNS essentially fulfils the initial expectations although in a reduced domain and provides data for turbulence-modelling studies, for instance by extracting an effective eddy viscosity from it. The most noticeable remaining disagreement with experiment is over the Reynolds shear stress.]]>
机译:<![cdata [ <标题>抽象 ara>在轴对称凹凸上的bachalo-johnson实验是一个主要的验证案例自1980年代以来冲击边界层交互的湍流模型。在本作本作中,使用改进的延迟分离涡流模拟(IDDES)作为子网格级(SGS)和墙面模型,进行了该流程的壁图的大涡模拟(WMLE),具有合成湍流发生器,期待与实验接近足够的协议。然而,即使在震荡位置而言,莫尔斯的结果也令人失望,即使来自两个网格的结果,也是4.7×10 <上标> 8 和1.6×10 <上标> 9 单元格的同意彼此友好。这种网格精制的失败是为了警告不准确的模拟是非常关注的,并且探索了它的原因。然后,我们进行了嵌入在LES上的直接数值模拟(DNS),在缩小的域中,具有8×10 <上标> 9 网格单元。 DNS具有更准确的冲击位置和整体压力分布。良好的压力梯度的皮肤摩擦也远高于LES;因此,宽差出现在冲击波的上游,大部分可能引起的快速加速度导致非典型剪切应力曲线。尝试了其他SGS模型,而且比IDDES更糟糕。 DNS基本上满足了初始期望,尽管在降低的域中,并且提供了湍流建模研究的数据,例如通过从中提取有效的涡流粘度。与实验最明显的剩余分歧是雷诺剪切应力。 ]]>

著录项

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