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Experimental and numerical study of heat transfer downstream of an axisymmetric abrupt expansion and in a cavity of a circular tube

机译:轴对称突变体下游和圆管腔内传热的实验和数值研究

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This research is an experimental and numerical investigation of heat transfer and fluid flow characteristics in separated, recirculated and reattached regions created by an axisymmetric abrupt expansion and by an abrupt expansion followed by an abrupt contraction (called a “cavity”) in a circular tube at a uniform wall temperature. The flow just upstream of the expansion was unheated and proved to be fully-developed at the entrance to the heated cavity region. Local heat transfer coefficients were measured using a balance-type isothermal heat flux gage. Measurements were made at a small-to-large tube diameter ratio of d/D = 0.4 and downstream Reynolds numbers ranging from ReD = 4,300 to 44,500. Generally, the maximum Nusselt numbers downstream of an axisymmetric abrupt expansion at a uniform wall temperature occur between 9 and 12 step heights from the expansion step. Numerical simulation has been carried out by a two-equation turbulence model and its results such as mean velocity profiles and local Nusselt numbers are in good agreement with experimental results.
机译:这项研究是对分离,再循环和再附着区域中的传热和流体流动特性进行的实验和数值研究,这些区域由轴对称的突然膨胀和突然的膨胀随后突然收缩(称为“腔”)在圆形管中产生。均匀的壁温。膨胀上游的流动未被加热,并在加热腔区域的入口处被充分发展。使用平衡式等温热通量规测量局部传热系数。在d / D的大/小直径比= 0.4的情况下进行测量,下游的雷诺数范围为Re D = 4,300至44,500。通常,在均匀壁温下,轴对称突然膨胀下游的最大Nusselt数出现在距离膨胀步骤9到12的台阶高度之间。通过两方程湍流模型进行了数值模拟,其结果(例如平均速度剖面和局部Nusselt数)与实验结果非常吻合。

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