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Three-dimensional vorticity measurements in the wake of a yawed circular cylinder

机译:偏航圆柱体后的三维涡度测量

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Using a phase-averaged technique, the dependence of the wake vortical structures on cylinder yaw angle alpha (=0 degrees-45 degrees) was investigated by measuring all three-velocity and vorticity components simultaneously using an eight-hot wire vorticity probe in the intermediate region (x/d=10) of a yawed stationary circular cylinder wake. For all yaw angles, the phase-averaged velocity and vorticity contours display apparent Kaacutermaacuten vortices. It is found that when alpha < 15 degrees, the maximum coherent concentrations of the three vorticity components do not change with alpha. However, when alpha is increased to 45 degrees, the maximum concentrations of the coherent transverse and spanwise vorticity components decrease by about 33% and 50%, respectively, while that of the streamwise vorticity increases by about 70%, suggesting that the strength of the Kaacutermaacuten vortex shed from the yawed cylinder decreases and the three dimensionality of the flow is enhanced. The maximum coherent concentrations of u and v contours decrease by more than 20% while that of w increases by 100%. Correspondingly, the coherent contributions to the velocity variances u(2) and v(2) decrease, while that of w(2) increases. These results may indicate the generation of the secondary axial vortices in yawed cylinder wakes when alpha is larger than 15 degrees. The incoherent vorticity contours omega(2)(xr) are stretched along an axis inclining to the x-axis at an angle beta in the range of 60 degrees-25 degrees for alpha=0 degrees-45 degrees. The magnitudes of root omega(2)(xr)(*) and root omega(2)(yr)(*) through the saddle points are comparable to the maximum concentration of the coherent spanwise vorticity omega approximate to(*)(z) at all cylinder yaw angles, supporting the previous speculation that the strength of the riblike structures in the cylinder wake is about the same as that of the spanwise structures, even in the yawed cylinder wakes.
机译:使用相位平均技术,通过使用中间的八热​​线涡旋探头同时测量所有三个速度和涡旋分量,研究了尾流涡旋结构对圆柱偏航角α(= 0度-45度)的依赖性。偏航固定圆柱尾流的区域(x / d = 10)。对于所有偏航角,相位平均速度和涡度等高线均显示出明显的Kaacutermaacuten涡旋。发现当α<15度时,三个涡度分量的最大相干浓度不会随α改变。但是,当α增加到45度时,相干的横向涡旋分量和展向涡旋分量的最大浓度分别降低约33%和50%,而流向涡旋分量的最大浓度分别增大约70%,这表明从偏航圆柱体喷出的Kaacutermaacuten涡流减少,流动的三维增强。 u和v等高线的最大相干浓度降低超过20%,而w的最大相干浓度增加100%。相应地,对速度变化《 u(2)》和《 v(2)》的相关贡献减小,而对《 w(2)》的速度变化的相关贡献增加。这些结果可能表明,当alpha大于15度时,在偏航的圆柱尾流中会产生次级轴向涡流。不相干的涡旋轮廓 omega(2)(xr)沿相对于x轴倾斜的轴以60度至25度范围内的角度β(对于alpha = 0度至45度)拉伸。通过鞍点的根 omega(2)(xr)(*)和根 omega(2)(yr)(*)的大小与相干展向涡度ω的最大浓度相当在所有圆柱偏航角下近似于(*)(z),支持先前的推测,即即使在偏航圆柱尾流中,圆柱尾流中肋状结构的强度也与翼展方向结构的强度大致相同。

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