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Experimental study on a yawed square cylinder in oscillatory flows

机译:横摆偏摆的实验研究

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摘要

The vortical structures around a yawed square cylinder oscillating in quiescent water are investigated using the particle image velocimetry technique. Following a previous study on the hydrodynamics (Lou et al., 2017), the present experiments are performed at different yaw angles (alpha) and Keulegan-Carpenter (KC) numbers to correlate the independence principle (IP) to vortical flow structures. At KC = 6, the vortex pair shows no shedding. Similar vortex patterns at different yaw angles result in similar hydrodynamic behaviors, which validates the IP at small KC numbers. The single and double pairs of vortex shedding regimes are observed for alpha = 0 degrees at KC = 11 and 19, respectively, and the vortex shedding process is determined by the movement of the cylinder as well as the interaction between vortices and shear layers. As alpha increases to 45 degrees, the shear layers are stretched and show attachment to the upper and lower sides of the cylinder for most of the time within one oscillating cycle. The shedding is only observed at the end of each half cycle and the vortices are found to reattach to the cylinder body. The subsequent drag force behavior of the yawed cylinder displays significant differences from that at alpha = 0 degrees and hence the IP is no longer applicable at KC = 11 and 19. When KC increases to 25, a three pairs of vortex shedding regime can be observed at both alpha = 0 degrees and 45 degrees. A similar flow feature, characterized by the shear layer attachment when the cylinder is at the neutral position and the vortex shedding at the end of each half cycle, has been found for both alpha = 0 degrees and 45 degrees. This result indicates that the IP becomes valid for the yawed square cylinder when the KC is sufficiently large until it is analogous to the steady flow.
机译:使用粒子图像测速技术研究了在静止水中振荡的偏航方筒周围的旋涡结构。在先前对流体动力学的研究(Lou等人,2017)之后,本实验在不同的偏航角(α)和Keulegan-Carpenter(KC)数下进行,以将独立原理(IP)与旋涡流结构相关联。在KC = 6时,涡旋对没有脱落。在不同的偏航角上相似的涡旋模式会导致相似的流体动力学行为,从而在较小的KC数下验证了IP。在KC = 11和19时,α= 0度分别观察到单对涡旋脱落和双涡旋脱落,而涡旋脱落的过程取决于圆柱体的运动以及涡旋与剪切层之间的相互作用。随着Alpha增大到45度,剪切层会拉伸,并在一个振荡周期的大部分时间内显示附着在圆柱体的上侧和下侧。仅在每个半周期结束时才观察到脱落,并且发现涡旋会重新附着到圆柱体上。偏航圆柱体随后的拖曳力行为与alpha = 0度时表现出显着差异,因此IP不再适用于KC = 11和19。当KC增加到25时,可以观察到三对涡旋脱落状态在alpha = 0度和45度处。对于α= 0度和45度,都发现了类似的流动特征,其特征是当圆柱体处于中性位置时剪切层附着,并且在每个半周期结束时涡旋脱落。该结果表明,当KC足够大直到类似于稳定流时,IP对偏航方筒才有效。

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