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Experimental Investigation of Flow Separation Control Using an Array of Synthetic Jets

机译:使用一列合成射流进行分流控制的实验研究

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An experimental study of flow control using an array of three synthetic jets has been undertaken in a separated laminar flow over an inclined flat plate in a water channel. Particle image velocimetry was employed to obtain the information about the extent of flow separation delay at different synthetic jet operating conditions. A laser-induced florescence flow visualization technique was used to reveal the characteristics of the vortical structures produced by the synthetic jets, which result in a delay of separation. It was observed that the flow separation delay is typically associated with the presence of two or three streaks of high streamwise velocity in the separated flow. Based on the results from the present experiment, a parameter map indicating the flow patterns observed at different synthetic jet operating conditions is produced. In addition, a contour map showing the separation control effectiveness at the corresponding conditions is also obtained. It was found that the two-streak flow pattern is mostly produced at a jet-to-freestream velocity ratio between 0.3 and 0.5, whereas the three-streak pattern occurs at a velocity ratio between 0.5 and 1.5. The laser-induced florescence images confirm that the two-streak flow pattern is caused by the hairpin type vortical structures produced by synthetic jets, whereas the three-streak pattern is caused by the tilted vortex ring type structures. For the range of actuator operating conditions tested in this study, operating the synthetic jets at a dimensionless stroke length of around 2, a velocity ratio of around 0.5, and a Strouhal number of around 1.6 would deliver the best flow control effect with the least energy consumption. Under these conditions, hairpinlike vortical structures are observed with a streamwise spacing of 44% of the local boundary-layer thickness at the orifices of the synthetic jets. In this experiment, the spacing between the jets and the distance between the jet array and the baseline separation line are fixed. As the level of interaction between neighboring synthetic jets and their flow control effectiveness are expected to alter upon changes in these two parameters, the generality of this finding remains to be established in future work.
机译:使用三个合成射流的阵列进行流量控制的实验研究已在水通道中倾斜平板上方的分离层流中进行。采用颗粒图像测速仪获得有关在不同合成射流操作条件下流分离延迟程度的信息。使用激光诱导的荧光流动可视化技术来揭示合成射流产生的涡旋结构的特征,这会导致分离延迟。观察到,流分离延迟通常与分离的流中存在两个或三个流向速度高的条纹有关。根据本实验的结果,将生成一个参数图,该参数图指示在不同的合成射流操作条件下观察到的流动模式。另外,还获得了示出在相应条件下的分离控制有效性的轮廓图。已经发现,两条纹的流型主要以射流与自由流的速度比在0.3和0.5之间产生,而三条纹的流型则以0.5和1.5的速度比出现。激光诱导的荧光图像证实,两条纹的流动模式是由合成射流产生的发夹型旋涡结构引起的,而三条纹的模式是由涡旋环型结构的倾斜引起的。在本研究中测试的执行器操作条件范围内,以约2的无因次行程长度,约0.5的速度比和1.6的斯特劳哈尔数操作合成射流将以最小的能量提供最佳的流量控制效果消费。在这些条件下,观察到发夹状的旋涡结构,在合成射流的孔口处,流向间距为局部边界层厚度的44%。在该实验中,射流之间的间距以及射流阵列与基线分隔线之间的距离是固定的。由于相邻的合成射流之间的相互作用水平及其流量控制效果预计会因这两个参数的变化而改变,因此,这一发现的普遍性仍有待在以后的工作中确立。

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