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Computational Analysis of Interaction of a Sweeping Jet with an Attached Crossflow

机译:清扫射流与附加横流相互作用的计算分析

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摘要

Computational-fluid-dynamics-based simulations are conducted to investigate the interaction of a sweeping jet generated by a fluidic oscillator with an attached turbulent crossflow. Improved delayed detached-eddy simulation is employed as a practical yet high-fidelity turbulence modeling approach to resolve the flow structures inside the oscillator's passages and in the crossflow region. The predicted flow generated by an oscillator with an outlet hydraulic diameter of 10 mm using air as a working fluid is validated against the particle image velocimetry data for two jet-to-freestream velocity ratios of 1 and 3. Close agreement is observed between the current numerical study and experimental data for the time-averaged and time-resolved flowfields at both velocity ratios. Formation of a pair of counter-rotating streamwise vortices is observed with a growth in its strength and size as the jet velocity increases. A greater penetration of the jet in both normal and lateral directions at higher jet velocity is also seen.
机译:进行了基于计算流体动力学的模拟,以研究由流体振荡器产生的清扫射流与附加的湍流交叉流的相互作用。改进的延迟分离涡模拟被用作一种实用而又高保真的湍流建模方法,以解决振荡器通道内部和错流区域的流动结构。针对两个射流与自由流速度比为1和3的粒子图像测速数据,验证了使用空气作为工作流体的出口液压直径为10 mm的振荡器产生的预测流量。两种速度比下的时间平均和时间分辨流场的数值研究和实验数据。观察到一对反向旋转的涡流的形成,其强度和尺寸随着射流速度的增加而增加。在较高的射流速度下,还可以看到射流在法向和横向方向上都有更大的穿透力。

著录项

  • 来源
    《AIAA Journal》 |2019年第2期|682-695|共14页
  • 作者

    Aram Shawn; Shan Hua;

  • 作者单位

    Naval Surface Warfare Ctr, Carderock Div, West Bethesda, MD 20817 USA;

    Naval Surface Warfare Ctr, Carderock Div, West Bethesda, MD 20817 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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