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Characteristics of the free-end mean pressure distribution for a surface-mounted finite-height cylinder

机译:表面安装有限高度圆筒的自由端平均压力分布的特性

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Wind tunnel experiments at a Reynolds number of Re = 6.5 × 10~4 were used to study the effect of aspect ratio and boundary layer thickness on the mean static pressure distribution on the free end of a surface-mounted finite-height cylinder. The cylinders aspect ratio was changed in small increments from AR = 0.5 to AR = 11. Two different boundary layer thicknesses (relative to the cylinder diameter) were employed, S/D = 0.6 and 5/ D = 1.9. From analysis of the mean pressure contour plots, it was found that the sizes and locations of regions of lower pressure, adverse pressure gradient, and higher pressure, and the appearance of "eye-like spots", are sensitive to both AR and S/D. The adverse pressure gradient occurs just ahead of the mean reattachment line while the eye-like spots are related to termination points of the legs of the arch vortex within the free-end mean recirculation zone. The total normal force coefficient experienced by the cylinder is strongly influenced by the contribution of the wall shear stress on the sides of the cylinder, with a change in direction of the net vertical shear stress contribution occurring between AR = 7 and AR = 8 for both boundary layers.
机译:Reynolds Re = 6.5×10〜4的风洞实验用于研究纵横比和边界层厚度对表面安装有限高度圆筒的自由端上的平均静压分布的影响。汽缸纵横比从Ar = 0.5到Ar = 11的小增量改变。采用两个不同的边界层厚度(相对于汽缸直径),S / D = 0.6和5 / d = 1.9。从分析平均压力轮廓图中,发现较低压力,不利的压力梯度和更高压力的区域的尺寸和位置,以及“眼睛状点”的外观对AR和S / S / S / S /)敏感D.不利的压力梯度在平均重新连接线之前发生,而眼睛状斑点与自由端平均再循环区域内的拱涡体的腿的端接点相关。汽缸经历的总法正常力系数受到壁剪切应力在圆筒侧面上的贡献的强烈影响,随着ar = 7和ar = 8之间发生的净垂直剪切应力贡献方向的变化边界层。

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