LES Investigation of a Piston-driven Synthetic Jet Actuator with Multiple Orifices

Q2 Mathematics
Tung Duy Pham, Tomoaki Watanabe, K. Nagata
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引用次数: 0

Abstract

A piston-driven synthetic jet actuator has the potential for application in flow control and fundamental studies of turbulence, although the high-speed flow generated by this actuator is less investigated than a low-speed synthetic jet. The interaction of high-speed jets issued from a piston-driven synthetic jet actuator with multiple orifices is investigated with large eddy simulation (LES). The maximum jet Mach number is related to the maximum pressure inside the actuator regardless of the number of orifices. Temporal variations of the jet Mach number are almost identical for different cycles, and the jet formation in each cycle occurs under the same conditions despite the unsteady nature of the jet interaction. The phase-averaged statistics are used to examine the interaction of the synthetic jets. The converging, merging, and combined regions known for the interaction of continuous jets appear for the interaction of the high-speed synthetic jets slightly before the end of the blowing phase. However, the converging region is not clearly observed at the beginning of the blowing phase because the jets tend to be parallel to each other. Therefore, the combined region forms at a late stage of the blowing phase. Before the jets are combined, velocity fluctuations in the blowing phase become large near the furthest locations where the jets reach. Once the jets merge by their interaction, large velocity fluctuations are observed at the downstream end of the merging region. The probability density functions of velocity fluctuations in the blowing phase tend to deviate from a Gaussian distribution along the centerline of the jets. This deviation is more significant for the two-orifice model than for the four-orifice model under the same actuation frequency.
多孔活塞驱动合成射流致动器的 LES 研究
活塞驱动的合成射流致动器具有应用于流动控制和湍流基础研究的潜力,但与低速合成射流相比,对这种致动器产生的高速流动的研究较少。本文通过大涡流模拟(LES)研究了带有多个孔口的活塞驱动合成射流致动器产生的高速射流的相互作用。无论喷孔数量多少,最大射流马赫数都与致动器内部的最大压力有关。不同周期的射流马赫数的时间变化几乎相同,尽管射流相互作用具有不稳定性,但每个周期的射流形成条件相同。相平均统计量用于研究合成射流的相互作用。在吹气阶段结束前,高速合成射流的相互作用出现了已知的连续射流相互作用的会聚、合并和组合区域。然而,在吹气阶段开始时,由于喷流往往相互平行,因此无法清楚地观察到会聚区。因此,汇合区是在吹气阶段的后期形成的。在射流合并之前,吹气阶段的速度波动在射流到达的最远位置附近变得很大。一旦喷流在相互作用下合并,在合并区域的下游端就会观察到较大的速度波动。吹气阶段速度波动的概率密度函数沿射流中心线倾向于偏离高斯分布。在相同的驱动频率下,这种偏差在双喷口模型中比在四喷口模型中更为明显。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CFD Letters
CFD Letters Chemical Engineering-Fluid Flow and Transfer Processes
CiteScore
3.40
自引率
0.00%
发文量
76
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