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Numerical study of flow physics in supersonic base-flow with mass bleed

机译:超音速渗流渗流的数值模拟。

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摘要

Large Eddy Simulation (LES) with dynamic sub-grid scale eddy viscosity model has been applied to numerically investigate the evolution of complicated flow structures in supersonic base flow with mass bleed. Mean flow properties obtained from numerical simulations, such as axial velocity, pressure on the base surface, have been compared with the experimental measurements to show that LES is able to predict the mean flow properties with acceptable accuracy. The data obtained from LES has been further analyzed to understand the evolution of coherent structures in the flow field. Periodical shedding of vortical structures from the outer shear layer has been observed and it has also been found that this vortex shedding is associated with the flapping of the outer shear layer. The frequency of flapping of the outer shear layer has been found out and the phase-averaged streamlines have been analyzed to further study the evolution of vortical structures associated with this flapping. The phase-averaged streamline plots clearly elucidate the evolution of vortical structures along the outer shear layer. Further, the study of these structures is investigated by performing Proper Orthogonal Decomposition (POD) analysis of the data, obtained along the central plane in the wake region. The POD results also seem to agree well with the observations made in the phase averaged streamline plots, as the concentrated energy and enstropy are observed in the outer shear layer with fewer POD modes. (C) 2016 Elsevier Masson SAS. All rights reserved.
机译:具有动态子网格规模涡粘性模型的大型涡模拟(LES)已被用于数值研究具有渗流的超声速基流中复杂流动结构的演化。从数值模拟获得的平均流量特性,例如轴向速度,基面上的压力,已与实验测量值进行了比较,以表明LES能够以可接受的精度预测平均流量特性。进一步分析了从LES获得的数据,以了解流场中相干结构的演变。已经观察到周期性的涡旋结构从外部剪切层脱落,并且还发现这种涡旋脱落与外部剪切层的拍打有关。找出了外剪切层扑动的频率,并分析了相平均流线,以进一步研究与该扑动有关的旋涡结构的演化。相平均流线图清楚地阐明了沿外剪切层的旋涡结构的演化。此外,通过对沿尾流区域中心平面获得的数据进行适当的正交分解(POD)分析,研究了这些结构。 POD结果似乎也与在相位平均流线图中所做的观察很好地吻合,因为在POD模式较少的外剪切层中观察到了集中的能量和熵。 (C)2016 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2016年第11期|1-17|共17页
  • 作者

    Das Pratik; De Ashoke;

  • 作者单位

    Indian Inst Technol, Dept Aerosp Engn, Kanpur 208016, Uttar Pradesh, India;

    Indian Inst Technol, Dept Aerosp Engn, Kanpur 208016, 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

    LES; Supersonic base bleed; POD;

    机译:LES;超音速流血;POD;

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