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Large-Eddy Simulation of Flow over a Wall-Mounted Hump with Separation and Reattachment

机译:带有分离和重新连接的壁挂式驼峰上的大涡模拟

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摘要

Wall-resolved large-eddy simulation of a model turbulent flow involving favorable and adverse pressure gradients, imposed by surface curvature of a wall-mounted hump, is performed for a spanwise-periodic computational domain. The flow acceleration over the front portion of the hump is strong enough to exceed the relaminarization criterion of Narasimha and Sreenivasan ("Relaminarization in Highly Accelerated Turbulent Boundary Layers," Journal of Fluid Mechanics, Vol.61, No.3, 1973, pp.417-447) but only over a relatively short streamwise extent. Although the flow does not relaminarize, turbulent skin-friction variation exhibits a plateau, also observed in the experiment of Greenblatt etal. ("A Separation Control CFD Validation Test Case, Part 1: Baseline and Steady Suction," AIAA Journal, Vol.44, No.12, 2006, pp.2820-2830), before it again continues to rise. The subsequent adverse pressure gradient is strong enough to cause flow separation. The location and extent of flow separation, including skin-friction distributions, compare reasonably well with experimental data. Computed velocity and Reynolds stress profiles are also compared with the experimental results. A systematic study of the effect of computational domain span, subgrid-scale model, tunnel backpressure, incoming boundary layer, grid refinement, Mach number, and top tunnel wall contour (which models the blockage effect of the experimental setup) is carried out, and sensitivity of the results to these parameters is discussed.
机译:对于跨周期的计算域,对壁面解析大涡模拟,该模型涉及由壁挂式驼峰的表面曲率强加的有利和不利压力梯度的湍流模型。驼峰前部的流动加速度足够强,足以超过Narasimha和Sreenivasan的再分层标准(“高度加速的湍流边界层中的再分层”,《流体力学》,第61卷,第3期,1973年,第pp。 417-447),但仅在相对较短的流范围内。尽管流动没有重新分层,但是湍流的皮肤摩擦变化表现出平稳状态,这也在Greenblatt等人的实验中观察到。 (“ AAA分离控制CFD验证测试用例,第1部分:基线和稳定抽吸”,AIAA杂志,第44卷,第12期,2006年,第2820-2830页),然后再次上升。随后的不利压力梯度足够强以引起流动分离。流动分离的位置和程度(包括皮肤摩擦分布)与实验数据进行了比较合理的比较。计算的速度和雷诺应力曲线也与实验结果进行了比较。对计算域跨度,子网格规模模型,隧道背压,进入边界层,网格细化,马赫数和顶部隧道壁轮廓(用于模拟实验装置的阻塞效应)的影响进行了系统研究,并且讨论了结果对这些参数的敏感性。

著录项

  • 来源
    《AIAA Journal》 |2018年第2期|715-730|共16页
  • 作者

    Uzun Ali; Malik Mujeeb R.;

  • 作者单位

    Natl Inst Aerosp, Hampton, VA 23666 USA;

    NASA, Computat AeroSci Branch, Langley Res Ctr, MS 128, Hampton, VA 23681 USA;

  • 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

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