A Study of spatiotemporal features of sweeping jets acting on afterbody vortices using low-operation-rate stereo PIV

IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Experimental Thermal and Fluid Science Pub Date : 2024-06-05 DOI:10.1016/j.expthermflusci.2024.111244
Xiaodong Chen , Shan Zhong , Ozgun Ozer , Andrew Kennaugh , Tanghong Liu , Guangjun Gao
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Abstract

Although low-operation-rate particle image velocimetry (PIV) provides a good spatial accuracy in measurements at relatively affordable costs, it faces some challenges in capturing unsteady features of oscillatory flow. In this paper, a single sweeping jet actuated to control afterbody vortices from a 30 slanted-base cylinder is investigated at a Reynolds number of 87,000. Phase-locked stereo PIV measurements combining triggering reference obtaining and real-time processing via field programmable gate array (FPGA) are leveraged to reveal the unsteady characteristics of the sweeping jet. The examined cases show that the phase-locked method can well identify jet’s spatiotemporal development process in each oscillation cycle. A sinusoidal-like interaction along phases between the jet and the afterbody vortex can be reasonably detected. At each moment, coherent small vortical structures form at the upper and bottom jet/ambient interfaces, which are caused by Kelvin-Helmholtz instability. Since the induced vortex has the same rotation direction as the afterbody vortex on each side, they merge with each other as the jet approaches the vortex, causing an increase in vorticity. Meanwhile, the sweeping jet’s intrusion into the vortex region induces a rise in turbulent kinetic energy in that area, causing turbulence ingestion of the vortex which weakens the velocity gradient. The sweeping behavior of the jet dominates the afterbody vortex to meander as the jet pushes its way underneath the vortex. The findings of this study provide encouraging evidence for future applications of sweeping jets in control of afterbody vortices.

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利用低运行速率立体 PIV 研究作用于后机身涡流的扫掠射流的时空特征
虽然低操作速率粒子图像测速仪(PIV)能以相对低廉的成本提供良好的空间测量精度,但它在捕捉振荡流的非稳态特征方面面临一些挑战。本文研究了在雷诺数为 87,000 的条件下,为控制来自 30◦ 斜底气缸的后体涡流而驱动的单一扫掠射流。通过现场可编程门阵列 (FPGA) 结合触发参考获取和实时处理的锁相立体 PIV 测量,揭示了横扫射流的不稳定特性。研究结果表明,锁相法能够很好地识别喷气机在每个振荡周期中的时空发展过程。可以合理地检测到喷流与后体涡旋之间沿相位的正弦交互作用。在每一时刻,上、下喷流/环境界面上都会形成由开尔文-赫尔姆霍兹不稳定性引起的相干小涡旋结构。由于诱导漩涡与两侧的后体漩涡具有相同的旋转方向,因此当射流接近漩涡时,它们会相互融合,导致涡度增加。同时,横扫射流侵入涡旋区域会导致该区域的湍流动能上升,造成涡旋的湍流吞噬,从而减弱速度梯度。当射流从涡旋下方推进时,射流的横扫行为会主导后体涡旋的蜿蜒曲折。这项研究的结果为今后在控制后机身涡流中应用扫掠射流提供了令人鼓舞的证据。
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来源期刊
Experimental Thermal and Fluid Science
Experimental Thermal and Fluid Science 工程技术-工程:机械
CiteScore
6.70
自引率
3.10%
发文量
159
审稿时长
34 days
期刊介绍: Experimental Thermal and Fluid Science provides a forum for research emphasizing experimental work that enhances fundamental understanding of heat transfer, thermodynamics, and fluid mechanics. In addition to the principal areas of research, the journal covers research results in related fields, including combined heat and mass transfer, flows with phase transition, micro- and nano-scale systems, multiphase flow, combustion, radiative transfer, porous media, cryogenics, turbulence, and novel experimental techniques.
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