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Dissimilarity between the velocity and temperature fields in a perturbed turbulent thermal boundary layer

机译:扰动的湍流热边界层中速度和温度场之间的差异

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Dissimilarity between the streamwise velocity and temperature fields is investigated in a perturbed turbulent thermal boundary layer using direct numerical simulation. Perturbations are provided into a turbulent boundary layer by uniform blowing or suction from a spanwise slot. The skin-friction coefficient and Stanton number are significantly changed due to blowing and suction. The streamwise evolution of the Stanton number is very different from that of the skin-friction coefficient because the pressure gradient induced by blowing or suction plays an important role in the momentum transport. Before the slot, the mean streamwise velocity changes smoothly, as compared to the mean temperature, due to the pressure gradient, and a similar behavior is also observed in the variations of the streamwise velocity and temperature fluctuations. Above the slot, the change in the mean streamwise velocity is smaller than that in the mean temperature, and after the slot the mean streamwise velocity recovers slowly to the unperturbed flow as compared to the mean temperature. By investigating each term in the mean streamwise velocity and temperature budgets, it is concluded that the mean pressure gradient is the main source of dissimilarity between the mean streamwise velocity and temperature fields. The budgets for the variances of the streamwise velocity and temperature fluctuations show that the difference between the production terms in both budget equations, which results from the existence of the mean pressure gradient, is the primary source of dissimilarity between the streamwise velocity and temperature fields above the slot, whereas downstream of the slot, the velocity pressure-gradient term (i.e., pressure gradient fluctuation) is another important source of dissimilarity. Dissimilarity between the streamwise velocity and temperature fluctuations caused by blowing persists longer in the streamwise direction than that by suction. (C) 2001 American Institute of Physics. [References: 32]
机译:使用直接数值模拟研究了扰动的湍流热边界层中沿流速度和温度场之间的差异。通过沿翼展方向的缝隙均匀地吹气或吸气,将扰动提供给湍流边界层。由于吹气和吸气,皮肤摩擦系数和斯坦顿数显着改变。 Stanton数的沿流方向的变化与皮肤摩擦系数的变化非常不同,因为吹气或吸气引起的压力梯度在动量传递中起重要作用。在缝隙之前,由于压力梯度,与平均温度相比,平均水流速度平稳变化,并且在水流速度和温度波动的变化中也观察到类似的行为。在缝隙上方,平均流向速度的变化小于平均温度的变化,并且在缝隙之后,与平均温度相比,平均流向速度缓慢恢复到不受扰动的流量。通过研究平均流速和温度预算中的每个项,可以得出结论,平均压力梯度是平均流速和温度场之间差异的主要来源。流向速度和温度波动方差的预算表明,两个预算方程中生产项之间的差异是由平均压力梯度的存在引起的,是上述流向速度和温度场之间差异的主要来源。在缝隙中,而在缝隙的下游,速度压力梯度项(即压力梯度波动)是另一个重要的差异来源。由吹动引起的气流速度和温度波动之间的差异在气流方向上的持续时间长于吸力。 (C)2001美国物理研究所。 [参考:32]

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