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Upstream penetration behavior of the developed counter flow jet resulting from multiple jet impingement in the crossflow of cylindrical duct

机译:圆柱管横流中多次射流撞击导致发达逆流射流的上游渗透行为

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摘要

Experimental and numerical investigations of ultimate upstream penetration of developed counter flow jet formed as result of impingement of multiple round jets radially injected into a high-temperature confined crossflow have been performed. These investigations aimed to reveal an influence of strength of the developed counter flow jet on mixing intensity of jets in crossflow of cylindrical duct. Based on analysis of experimental data, the analytical dependence between dimensionless parameter of upstream penetration depth of counter flow jet and the square root of jets-to-mainstream momentum-flux ratio J has been established. The dependence proved to consist of linear region as well as nonlinear and asymptotic ones. For a given geometry an ultimate upstream penetration depth of the counter flow jet has been estimated to be approximately 2.1-2.3 diameter of the cylindrical duct. The corresponding value obtained on the base of numerical simulation turned out to be 1.8-2.0 diameter of the cylindrical duct. The dimensionless parameter h/D of radial jet penetration depth proved to be an appropriate to describe adequately an empirical character of upstream penetration of the counter flow jet within the linear region. Based on results of numerical simulation, axial velocity, temperature and pressure profiles as well as centerline turbulent kinetic energy contours have been obtained. It has been has also shown that an increase of the momentum-flux ratio promotes mixing in upstream recirculation flow zone and improves overall mixing performance as well.
机译:已经进行了实验和数值研究,该实验和数值研究是由于径向注入高温受限横流的多个圆形射流的撞击而形成的发达的逆流射流的最终上游渗透。这些研究旨在揭示发达的逆流射流强度对圆柱管横流中射流混合强度的影响。在实验数据分析的基础上,建立了逆流射流上游穿透深度的无量纲参数与射流与主流动量通量比J的平方根之间的解析相关性。事实证明,相关性包括线性区域以及非线性和渐近区域。对于给定的几何形状,逆流射流的最终上游穿透深度估计为圆柱管直径的约2.1-2.3。在数值模拟的基础上获得的相应值被证明是圆柱管的直径为1.8-2.0。径向射流穿透深度的无量纲参数h / D被证明是适当描述线性区域内逆流射流上游穿透的经验特性的合适方法。根据数值模拟的结果,获得了轴向速度,温度和压力曲线以及中心线湍动能轮廓。还已经表明,动量-通量比的增加促进了上游再循环流动区域中的混合并且还改善了整体混合性能。

著录项

  • 来源
    《International Journal of Heat and Mass Transfer》 |2018年第1期|1163-1178|共16页
  • 作者单位

    Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Institutskaya sir., 4/1, Novosibirsk 630090, Russia;

    Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Institutskaya sir., 4/1, Novosibirsk 630090, Russia;

    Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Institutskaya sir., 4/1, Novosibirsk 630090, Russia;

    Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Institutskaya sir., 4/1, Novosibirsk 630090, Russia;

    Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Institutskaya sir., 4/1, Novosibirsk 630090, Russia;

  • 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

    Impinging jets; Developed counter flow jet; Confined crossflow; Upstream penetration depth; Mixing;

    机译:射流撞击;开发逆流射流;受限的横流;上游渗透深度;混合;

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