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Zonal Overset-LES with stochastic volume forcing

机译:带随机音量强迫的Zoneal Overset-LES

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摘要

In this contribution, a hybrid Zonal LES tool is presented that uses a stochastic volume forcing for "inflow" turbulence generation. The here used hybrid approach is based on an implementation of the Non-Linear Perturbation Equations extended with fluctuating viscous terms, denoted as "Overset" since a perturbation analysis is performed on top of a background flow. A turbulent flat plate is considered to investigate the generation of inflow turbulence and how this artificial turbulence is seeded into the computational domain. At the inflow region, turbulence is stochastically generated (in three-dimensional space and time) with the Fast Random Particle-Mesh method and subsequently injected in the Overset-LES domain with the eddy-relaxation source term. This eddy-relaxation source term is shown to pilot the hydrodynamics while leaving the acoustics untouched (i.e., transparent for acoustic). The application of the Overset-LES method to a NACA0012 trailing edge at zero angle-of-attack is furthermore presented. Mean flow and turbulence characteristics in the wake show a good agreement with experimental data. Finally, a possible way to couple the turbulent sound sources into a CAA simulation is described. Comparison between directivities obtained with this method and reference data revealed good agreement.
机译:在此贡献中,提出了一种混合的Zonal LES工具,该工具使用随机体积强迫来生成“流入”湍流。这里使用的混合方法基于非线性波动方程的实现,该方程用波动的粘性项扩展,表示为“ Overset”,因为在背景流之上执行了波动分析。考虑使用湍流平板来研究流入湍流的产生以及如何将这种人工湍流播种到计算域中。在流入区域,使用快速随机粒子网格法随机地(在三维空间和时间中)生成湍流,然后用涡流松弛源项将其注入Overset-LES域。该涡流松弛源项被显示为在不影响声学的情况下引导流体力学(即,对声学透明)。此外,还介绍了Overset-LES方法在攻角为零的情况下对NACA0012后缘的应用。尾流中的平均流量和湍流特性与实验数据显示出良好的一致性。最后,描述了将湍流声源耦合到CAA模拟中的可能方法。通过这种方法获得的方向性与参考数据之间的比较显示出很好的一致性。

著录项

  • 来源
    《International Journal of Heat and Fluid Flow》 |2018年第4期|336-347|共12页
  • 作者单位

    TU Braunschweig, Inst Fluid Mech ISM, Dept Mech Engn, Hermann Blenk Str 37, D-38108 Braunschweig, Germany;

    TU Braunschweig, Inst Fluid Mech ISM, Dept Mech Engn, Hermann Blenk Str 37, D-38108 Braunschweig, Germany;

    German Aerosp Ctr DLR, Inst Aerodynam & Flow Technol, Dept Tech Acoust, Lilienthalpl 7, D-38108 Braunschweig, Germany;

    German Aerosp Ctr DLR, Inst Aerodynam & Flow Technol, Dept Tech Acoust, Lilienthalpl 7, D-38108 Braunschweig, 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
  • 关键词

    Overset-LES; Volume forcing; Trailing-edge simulation;

    机译:Overset-LES;体积逼迫;边缘仿真;
  • 入库时间 2022-08-18 02:59:41

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