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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Evolution of the turbulenton-turbulent interface of an axisymmetric turbulent jet
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Evolution of the turbulenton-turbulent interface of an axisymmetric turbulent jet

机译:轴对称湍流射流的湍流/非湍流界面的演变

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Measurements of a turbulent round air jet, using particle image velocimetry, were made to investigate the dynamics and transport processes at the continuous bounding interface between the turbulent and non-turbulent regions (T/NT) of the jet flow. The Reynolds number of the jet was in the range Red = 3,000-6,500 based on jet diameter with measurements taken between 0 and 40 jet diameters from the jet nozzle exit, which covers the developing and self-similar region of the jet. A velocity thresholding technique was used to define the T/NT interface. The results based on this methodology were found to agree well with previously published results (Westerweel et al. in Phys Rev Lett 95:174501, 2005; Westerweel et al. in J Fluid Mech 631:199-230, 2009; and Anand and Boersma in Exp Fluids 47:995-1007, 2009). The evolution of the turbulence characteristics at the interface was investigated using conditionally averaged axial velocity, azimuthal vorticity, turbulent intensity, and Reynolds shear stress. A distinct change in behavior is observed between the near-field region, 0 ≤ x/d ≤ 8, and the far-field, selfsimilar region, x/d > 20. Profiles of the conditional mean axial velocity demonstrate no clear jump in the conditional mean axial velocity at the interface for x/d < 8. However, the emergence of the jump is observed at x/d ≈ 8, and the magnitude of the jump continues to increase between 8 < x/d < 20 before reaching a steady value in the selfsimilar region, x/d > 20. All the scaled statistics show selfsimilar behavior downstream of x/d > 20. Similar behavior is observed for the peak in the azimuthal vorticity and the jump in the Reynolds shear stress profiles. The evolution of the rate of entrainment also confirms the creation and growth of the jump in the mean conditional velocity profiles in the developing region of the jet.
机译:使用粒子图像测速仪对湍流圆形空气射流进行了测量,以研究射流的湍流和非湍流区域(T / NT)之间的连续边界界面处的动力学和传输过程。射流的雷诺数基于射流直径在Red = 3,000-6,500范围内,并且从射流喷嘴出口的0到40个射流直径之间进行测量,该范围覆盖了射流的发育区域和自相似区域。速度阈值技术用于定义T / NT接口。发现基于这种方法的结果与先前发表的结果非常吻合(Westerweel等人,Phys Rev Lett 95:174501,2005; Westerweel等人,J Fluid Mech 631:199-230,2009;以及Anand和Boersma在Exp Fluids 47:995-1007,2009中)。使用条件平均轴向速度,方位涡度,湍流强度和雷诺剪切应力研究了界面处湍流特性的演变。在0≤x / d≤8的近场区域和x / d> 20的远场自相似区域之间观察到了行为的明显变化。 x / d <8时界面处的条件平均轴向速度。但是,在x / d≈8处观察到跳跃的出现,并且跳跃幅度在达到20。所有按比例缩放的统计数据均显示自x / d> 20下游的自相似行为。在方位涡度的峰值和雷诺剪切应力分布中的跳跃中也观察到相似的行为。夹带速率的变化也证实了射流发展区域中平均条件速度剖面中跳跃的产生和增长。

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