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Identification of thermally-tagged coherent structures in the zero pressure gradient turbulent boundary layer

机译:零压力梯度湍流边界层中热标记相干结构的识别

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摘要

A zero pressure gradient boundary layer over a flat plate is subjected to step changes in thermal condition at the wall, causing the formation of internal, heated layers. The resulting temperature fluctuations and their corresponding density variations are associated with turbulent coherent structures. Aero-optical distortion occurs when light passes through the boundary layer, encountering the changing index of refraction resulting from the density variations. Instantaneous measurements of streamwise velocity, temperature and the optical deflection angle experienced by a laser traversing the boundary layer are made using hot and cold wires and a Malley probe, respectively. Correlations of the deflection angle with the temperature and velocity records suggest that the dominant contribution to the deflection angle comes from thermally-tagged structures in the outer boundary layer with a convective velocity of approximately 0.8U∞. An examination of instantaneous temperature and velocity and their temporal gradients conditionally averaged around significant optical deflections shows behavior consistent with the passage of a heated vortex. Strong deflections are associated with strong negative temperature gradients, and strong positive velocity gradients where the sign of the streamwise velocity fluctuation changes. The power density spectrum of the optical deflections reveals associated structure size to be on the order of the boundary layer thickness. A comparison to the temperature and velocity spectra suggests that the responsible structures are smaller vortices in the outer boundary layer as opposed to larger scale motions. Notable differences between the power density spectra of the optical deflections and the temperature remain unresolved due to the low frequency response of the cold wire.
机译:平板上的零压力梯度边界层在壁的热条件下会发生阶跃变化,从而形成内部加热层。产生的温度波动及其相应的密度变化与湍流相干结构相关。当光穿过边界层时,由于密度变化而导致折射率发生变化,就会发生航空光学畸变。分别使用热线和冷线以及Malley探针分别对流过边界层的激光所经历的流向速度,温度和光学偏转角进行瞬时测量。偏转角与温度和速度记录的相关性表明,对偏转角的主要贡献来自外边界层中热标记的结构,对流速度约为0.8U∞。对瞬时温度和速度及其瞬时梯度进行有条件的平均检查,发现其在明显的光学偏转附近表现出与受热涡旋通过一致的行为。强烈的偏转与强烈的负温度梯度和强烈的正速度梯度相关,在此方向上,流速速度波动的符号会发生变化。光学偏转的功率密度谱揭示了相关的结构尺寸约为边界层厚度。与温度和速度谱的比较表明,与较大尺度的运动相反,负责任的结构在外边界层中的涡旋较小。由于冷线的低频响应,光学偏转的功率密度谱和温度之间的显着差异仍未解决。

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    Rought Rebecca Lynn;

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  • 年度 2013
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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