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Effect of surface topology on the galloping instability of rectangular cylinders

机译:表面拓扑对矩形气缸奔腾不稳定性的影响

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The effect of geometry on the transverse galloping instability of rectangular cylinders was studied experimentally for Reynolds numbers between 1,000 and 10,000. In particular, a comparison was made between a rectangular cylinder with rounded corners and a smooth surface, and the same baseline geometry with added surface topology synthesized from two-dimensional Fourier-modes. The effects of the topology amplitude and wavelength were investigated. From measurements of the normal (galloping direction) force coefficient variation with angle-of-attack, it was found that the added surface topology generally had a destabilizing effect relative to the smooth cylinder. At the lowest Reynolds number, the smooth cylinder was stable, while the cylinders with added topology were unstable with respect to galloping. For Reynolds numbers from 5,000 to 10,000, the added topology did not cause a similar instability. However, there was a monotonic increase in the slope of the normal force coefficient at zero angle-of-attack with increasing surface height amplitude, thus moving the geometry closer to the instability threshold. This effect diminished as Reynolds number increased. Overall, for the range of parameters investigated herein, whenever the cylinders with topology were unstable to soft or hard galloping, the larger topology exhibited more favorable galloping resistance characteristics than the one with smaller topology. Topology wavelength was found to have no effect on the galloping behavior of the cylinder for Reynolds numbers below 7500, and a moderate increase in the normal force slope at zero angle of attack with decreasing wavelength for larger Reynolds numbers. The latter effect was associated with an increase in the angle of attack at which the cylinder could become unstable to hard galloping.
机译:几何形状对矩形圆柱横向疾动力的影响,实验研究了1000至10,000的雷诺数。特别地,在具有圆角的矩形圆柱体和光滑的表面之间进行比较,以及与由二维傅里叶模式合成的表面拓扑相同的基线几何形状。研究了拓扑幅度和波长的影响。从正常(奔波方向)的测量力与攻击角度的力系数变化,发现添加的表面拓扑通常相对于平滑圆筒具有稳定的效果。在最低雷诺数,平滑圆筒稳定,而具有添加拓扑的气缸相对于疾驰是不稳定的。对于从500​​0到10,000的雷诺数,添加的拓扑没有导致类似的不稳定。然而,在零攻角的正起响起的沉降角度下,在零攻角幅度的斜率中存在单调增加,从而使几何形状更接近不稳定性阈值。随着雷诺数的增加,这种效果减少了。总的来说,对于本文研究的参数范围,每当具有拓扑的气缸不稳定到软或良好疾驰时,较大的拓扑表现出比具有较小拓扑的良好良好的良好疾驰的特性。发现拓扑波长对雷诺数的河流的良好行为没有影响到7500以下的河流,并且在零攻角处的正常力斜率的中等增加,具有较大的雷诺数的波长。后一种效果与汽缸变得不稳定的攻击角度不稳定的效果有关。

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