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Steady-state and unsteady Reynolds-averaged Navier-stokes modelling of cold jets-in-hot crossflow in a cylindrical duct for non-impinging, impinging, and strongly impinging jets

机译:稳态和不稳定的雷诺瓦尔平均天Navier-Stokes在圆柱形管道中的冷喷气机 - 热十字流出,用于非撞击,撞击,强烈撞击喷气机

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摘要

The objective of this study is to demonstrate that strongly impinging jets-in-crossflow (JIC) will result in a counter flowing jet that will probably be unsteady. This numerical study was conducted in a 360° (complete cylindrical duct) computational domain using a steady-state Reynolds-Averaged Navier Stokes, RANS, and time-dependent URANS at various momentum-flux ratios J. Asymmetry in a steady-state RANS solution is very likely to be an indication of the flow's instability and unsteadiness. RANS predictions clearly show asymmetry in cases of strongly impinging jets. RANS solutions show that steady-state solutions are not appropriate if the flow is, or is suspected to be, unsteady. RANS and URANS solutions for computational domains <360° will require boundary conditions at the edges of the computational domain and will not correctly represent the flow if it is unsteady even if the RANS solution converges. The results of this study are consistent with, and extend, the experimental and numerical results published earlier that were motivated by mixing in gas turbine combustors.
机译:本研究的目的是证明强烈撞击的喷气式飞机(JIC)将导致柜台流动喷射可能是不稳定的。该数值研究在360°(完整的圆柱形管道)计算结构域中使用稳态雷诺平均的Navier Stokes,Rans和时间依赖于各个动量的血液传递比率J.在稳态RANS溶液中的不对称性很可能是流动不稳定和不稳定的指示。 Rans预测清楚地显示了在强烈撞击喷射的情况下的不对称性。 Rans解决方案表明,如果流量是,或怀疑是不稳定的,则稳态解决方案是不合适的。计算域的RAN和URANS解决方案<360°将需要计算域边的边界条件,如果即使RAN Solution收敛也不是不稳定的,则不会正确表示流量。该研究的结果与先前发表的实验性和数值结果一致,通过在燃气轮机燃烧器中混合而发表的实验和数值结果。

著录项

  • 来源
    《Heat and mass transfer》 |2020年第7期|2285-2302|共18页
  • 作者

    E. V. Kartaev; J. D. Holdeman;

  • 作者单位

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

    JH Consulting 5228 Meadow Moss Lane North Ridgeville OH 44039 USA National Aeronautics and Space Administration John H. Glenn Research Center at Lewis Field Cleveland OH 44135 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

    Impinging jets; Counter flow jet; Confined crossflow; JIC; Cylindrical duct; Momentum-flux ratio; Mixing;

    机译:撞击喷气机;逆流射流​​;限制跨流;JIC;圆柱形管道;动量通量比;混合;

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