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Afterbody Effects on Axisymmetric Base Flows

机译:后轴效应对轴对称基流的影响

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摘要

The influence of an afterbody on an axisymmetric wake flow is investigated with two-component particle image velocimetry at a Reynolds number of Re-D = 6.7 . 10(4) based on the model diameter. The reattachment distance is found to vary from two to four step heights as the afterbody diameter is increased. Measurements performed on equivalent planar backward-facing step geometries reveal that the reattachment length scales similarly to a planar backward-facing step when the afterbody to main-body diameter ratio approaches unity. The distribution of turbulent normal and shear stresses reveals a progressive inhibition of the radial fluctuations for increasing afterbody diameter, whereas a proper orthogonal decomposition analysis highlights a concurrent weakening of the shear-layer flapping mode. For d/D <= 0.4, the frequency spectrum of the time coefficient of the first proper orthogonal decomposition mode appears associated with the wake flapping motion and peaks in the range of St(D) = 10(-3) -10(-2). This frequency is associated with the recirculating flow unsteadiness observed in the azimuthal plane of the wake. The configuration without afterbody features an additional contribution at St(D) = 0.2, which is associated with vortex shedding. The current results reveal the dependence of low-frequency unsteadiness upon changes in the afterbody diameter.
机译:在Re-D = 6.7的雷诺数下,用两组分颗粒图像测速法研究了后装对轴对称尾流的影响。 10(4)基于模型直径。随着后车身直径的增加,重新安装距离从2到4步高变化。在等效的平面向后台阶几何形状上进行的测量表明,当后身与主体直径之比接近统一时,重新连接长度的缩放比例与平面向后台阶相似。湍流法向应力和剪应力的分布揭示了径向波动的渐进抑制,以增加后车身直径,而适当的正交分解分析则突出了剪切层扑动模式的同时减弱。对于d / D <= 0.4,第一适当正交分解模式的时间系数的频谱出现与尾流拍打运动相关,并且峰值在St(D)= 10(-3)-10(-2)范围内)。该频率与在尾流的方位角平面中观察到的再循环流动的不稳定性有关。没有后身的配置在St(D)= 0.2时具有额外的贡献,这与涡旋脱落有关。当前的结果表明低频不稳定对后车身直径变化的依赖性。

著录项

  • 来源
    《AIAA Journal》 |2016年第8期|2285-2294|共10页
  • 作者单位

    Delft Univ Technol, Aerodynam Dept, Kluyverweg 2, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Aerodynam Dept, Kluyverweg 2, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Aerodynam Dept, Kluyverweg 2, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Aerodynam Dept, Kluyverweg 2, NL-2629 HS Delft, Netherlands;

  • 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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