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Direct numerical simulation of forced circular jets: Effect of varicose perturbation

机译:强制圆形射流的直接数值模拟:静脉曲张的影响

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摘要

Free circular jets at low and intermediate Reynolds numbers evolve through discrete transitions accompanied by the formation of large-scale structures. Understanding dynamics of coherent structures in free jets suggests control strategies that can be used to achieve enhanced spreading and mixing of the jet with the surrounding fluid. In the present work, an active control technique that alters the vortex dynamics in the jet is implemented close to the nozzle resulting in an effect over the entire flow field. Among techniques available for controL., the one based on (axisymmetric) varicose perturbation has been considered. The effect of perturbation on jet evolution and flow structures is examined via a computational approach. Direct numerical simulation (DNS) of incompressible, spatially developing circular jets is reported for a Reynolds number of 1000. The three-dimensional unsteady Navier-Stokes equations are solved by a high order spatial and temporal discretization scheme. For small-scale perturbation using Gaussian white noise, the jet undergoes transition in conformity with experiments. With varicose perturbation, excitation frequencies play a significant role in the evolution of circular jets. Excitation frequencies of 0.1 and 0.2 show the formation of a trailing jet. For a frequency of 0.2, the circular jet shows pairing of the shed vortices. With further increase in the excitation frequency, formation of strong secondary hairpin vortices at the far field is to be seen. Largest influence of excitation is seen for frequencies around the preferred mode value of 0.32. For A thick shear layer helps in formation of vortex ring that undergoes tearing while a thinner shear layer develops a stronger vortex ring.
机译:低雷诺数和中雷诺数的自由圆形射流通过离散跃迁演化,并伴随形成大型结构。了解自由射流中相干结构的动力学表明,可以采用控制策略来增强射流与周围流体的扩散和混合。在当前工作中,在喷嘴附近实施了一种主动控制技术,该技术可改变喷嘴中的涡流动力学,从而在整个流场上产生影响。在可用于控制的技术中,已经考虑了一种基于(轴对称)静脉曲张摄动的技术。通过计算方法检查了扰动对射流演化和流动结构的影响。报告了不可压缩的,在空间上发展的圆形射流的直接数值模拟(DNS),雷诺数为1000。三维非定常Navier-Stokes方程通过高阶时空离散方案求解。对于使用高斯白噪声的小规模扰动,射流会根据实验进行过渡。在静脉曲张扰动下,激发频率在圆形射流的演变中起着重要作用。激励频率为0.1和0.2表示尾随射流的形成。对于0.2的频率,圆形射流显示出涡流成对。随着激励频率的进一步增加,可以看到在远场形成了强大的次级发夹涡。对于优选模式值0.32附近的频率,激发的影响最大。对于较厚的剪切层,有助于形成涡旋环,使其经受撕裂,而较薄的剪切层则形成较强的涡流环。

著录项

  • 来源
    《International Journal of Heat and Fluid Flow》 |2013年第12期|524-541|共18页
  • 作者单位

    Department of Mechanical Engineering, Indian Institute of Technology Kanpur, Kanpur 208 016, Uttar Pradesh, India;

    Department of Mechanical Engineering, Indian Institute of Technology Kanpur, Kanpur 208 016, Uttar Pradesh, India;

    Department of Mechanical Engineering, Indian Institute of Technology Kanpur, Kanpur 208 016, Uttar Pradesh, India;

  • 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

    Circular jet; Instability; Axisymmetric forcing; DNS; Entrainment; Q-function;

    机译:圆形射流;不稳定;轴对称强迫;DNS;夹带;Q功能;
  • 入库时间 2022-08-18 02:59:58

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