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Vortex formation of a finite-span synthetic jet: effect of rectangular orifice geometry

机译:有限跨度合成射流的涡流形成:矩形孔几何形状的影响

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The formation and evolution of flow structures of a finite-span synthetic jet issuing into a quiescent flow were investigated experimentally using stereoscopic particle image velocimetry (SPIV). The effect of two geometrical parameters, the orifice aspect ratio and the neck length, were explored at a Strouhal number of 0.115 and a Reynolds number of 615. Normalized orifice neck lengths of 2, 4 and 6 and aspect ratios of 6, 12, and 18 were examined. It was found that the effect of the aspect ratio is much larger than the effect of the neck length, and as the aspect ratio increases the size of the edge vortices decreases and the presence of secondary structures is more evident. Moreover, axis switching was observed and its streamwise location increases as the aspect ratio increases. The effect of the neck length on the flow structures and the evolution of the synthetic jet was found to be secondary, where the effect was only in the very near field (i.e. close to the jet's orifice).
机译:利用立体粒子图像测速仪(SPIV),对有限静态合成射流向静态流动的流动结构的形成和演化进行了实验研究。研究了两个几何参数的影响:孔口长宽比和颈部长度,其斯特劳哈尔数为0.115,雷诺数为615。归一化孔口颈部长为2、4和6,长宽比为6、12和检查了18个。发现长宽比的影响远大于颈部长度的影响,并且随着长宽比的增加,边缘涡旋的尺寸减小,并且二级结构的存在更加明显。而且,观察到轴切换,并且其沿流的位置随着纵横比的增加而增加。发现颈部长度对流动​​结构和合成射流的演变的影响是次要的,其中该影响仅在非常近的场中(即,靠近射流的孔)。

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