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Experimental investigation of the free convection velocity boundary layer and plume formation region for a heated horizontal cylinder

机译:水平加热圆柱体自由对流速度边界层和羽流形成区域的实验研究

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Particle image velocimetry measurements were obtained in the free convection water flow around a heated horizontal cylinder for a Rayleigh number of 1.33 × 10~6 and a Prandtl number of 5.98. Radial and circumferential velocity were investigated within and just outside the velocity boundary layer in a vertical plane perpendicular to the cylinder axis. Radial and axial velocity were observed in the early plume development just above the top of the cylinder in a vertical plane parallel to and passing through the cylinder axis. The submersion depth of the top of the cylinder below the free water surface normalized by cylinder diameter ranged from H/D = 2 to 8, which includes depths for which the plume sways and meanders in periodic motion. The effects of plume swaying and meandering on the velocity boundary layer and plume formation were investigated. It was found that the approach flow outside the boundary layer was affected by penetrative convection caused by swaying and meandering of the plume even though there is no horizontal confinement. Measurements within the boundary layer as it nears the plume formation region and within the plume formation region itself reveal that penetrative zconvection in the approach flow altered the boundary layer and these effects propagated downstream into the plume formation region. The data therefore identified a feedback loop for which the plume fluid returns to the boundary layer sustaining the swayine motion. A direct cause of meandering was not determined.
机译:颗粒图像测速仪的测量是在加热的水平圆柱体周围的自由对流水流中进行的,瑞利数为1.33×10〜6,普朗特数为5.98。在垂直于圆柱轴的垂直平面中,在速度边界层之内和之外,研究了径向和圆周速度。在平行于并通过圆柱轴的垂直平面中,在圆柱顶部上方的早期羽状流中观察到径向和轴向速度。圆柱体顶部自由水面以下的圆柱体浸没深度通过圆柱体直径归一化,范围为H / D = 2到8,其中包括羽流以周期性运动摇摆和蜿蜒的深度。研究了羽流摇摆和弯曲对速度边界层和羽流形成的影响。结果发现,边界层外的进场流受到了羽流的摇摆和曲折引起的渗透对流的影响,即使没有水平约束也是如此。边界层靠近羽流形成区域时的测量以及羽流形成区域本身的测量表明,进场流中的渗透性z对流改变了边界层,并且这些影响向下游传播到羽流形成区域。因此,数据确定了一个反馈回路,羽流流体为此返回到边界层,以保持摇摆运动。尚未确定引起弯曲的直接原因。

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