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Pressure distributions on three circular cylinders in different equilateral-triangular arrangements at subcritical Reynolds Number

机译:亚临界雷诺数的不同等边三角形布置中的三个圆柱上的压力分布

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Pressure distributions on three circular cylinders in different equilateral-triangular arrangements were investigated by wind tunnel test at a subcritical Reynolds number of 5.5x10~4. The spacing ratios of their centers were in the range 1.7 <=N/d<=5.0. It has been shown that the angles of incident flow strongly in-fluence the pressure distributions on any one of the cylinders. Due to the interference of the shear layers and/or wakes, the most complex features of pressure distributions can be found on the cylinder located in downstream. As to the levels of interference regarding to the effect of spacing ratio, the results show mainly four different effect regions, i.e. effect of small, medium, transition and larger spacing can be identified. In small spacing, further more, three basic types of flow pattern can be classified due to various angles of incident flow. These are flow patterns of proximity effect, shear layer reattachment effect and wake effect.
机译:通过风洞试验在亚临界雷诺数为5.5x10〜4的情况下,研究了三个圆柱体上的三个圆柱体的压力分布。其中心的间距比率在1.7 <= n / d <= 5.0的范围内。已经表明,入射流的角度强烈流入任何一个气缸上的压力分布。由于剪切层和/或唤醒的干涉,可以在位于下游的汽缸上找到压力分布的最复杂的特征。关于对间距率的影响的干扰水平,结果主要显示四种不同的效果区,即可以识别较小,培养基,过渡和较大间距的效果。在小间隔中,由于各种入射流动的角度,可以分类三种基本类型的流动模式。这些是邻近效应的流动模式,剪切层重新连接效果和唤醒效果。

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