Dynamics of vortex interaction and entrainment characteristics in inclined elliptic jets using sparse track-enhanced volumetric measurements

IF 2.5 3区 工程技术 Q2 ENGINEERING, MECHANICAL
Xin Zeng, Hao Qu, Chuangxin He, Yingzheng Liu, Lian Gan
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引用次数: 0

Abstract

This work is a further discussion about elliptical jet flows (Zeng et al. in Exp Fluids 64:142, 2023) by exploring how variations in nozzle shape enhance flow control efficiency. The study examines the dynamic evolution of vortex interactions and their positive effects on the entrainment of inclined elliptical jets (with inclination angles of 30° in both the major and minor planes) compared to non-inclined elliptical jets. Experiments were conducted at an aspect ratio (AR) of 2 and a Reynolds number of approximately 3000. Time-resolved tomographic particle image velocimetry (Tomo-PIV) and three-dimensional Lagrangian particle tracking (3D LPT) measurements were employed to capture the flow dynamics in detail. The Eulerian velocity field datasets obtained from Tomo-PIV are enhanced using high-precision tracks from 3D LPT measurements, improving the accuracy of velocity field reconstruction. Statistical analyses indicate that inclined elliptical jets exhibit greater mass entrainment characteristics and higher momentum flux compared to non-inclined elliptical jets. The power spectral densities (PSDs) and time-domain spectral proper orthogonal decomposition (td-SPOD) results reveal that for the major-plane inclined-A nozzle, both the leading and trailing vortex rings share the same dominant frequency of St = 0.28, suggesting that vortex pairing and merging in the 30° inclined-A jet may be a periodic process. After vortex merging at approximately Y/De ≈ 3.5, the first axis-switching is completed, indicating that axial switching is suppressed in the major-plane inclined-A elliptical jet compared to the non-inclined case. In contrast, for the minor-plane inclined-B jet, the dominant frequencies of the leading and trailing vortex rings are St = 0.28 and St = 0.61, respectively. In some instances, two consecutive large-scale vortex rings corresponding to SPOD mode (3,4) do not merge downstream; instead, they develop independently and eventually break down separately. At the axis-switching plane (Y/De = 2.5), during both the merging and axis-switching processes of vortex rings in the two inclined nozzles, a significant number of streamwise vortex structures are generated. This phenomenon substantially contributes to an increased mean entrainment rate, further enhancing the mixing characteristics of inclined elliptical jets.

Graphical Abstract

斜椭圆射流中涡相互作用和夹带特性的稀疏轨迹增强体积测量
这项工作是通过探索喷嘴形状的变化如何提高流动控制效率来进一步讨论椭圆射流(Zeng et al. in Exp Fluids 64:142, 2023)。本研究考察了涡旋相互作用的动态演变,以及与非倾斜椭圆射流相比,涡旋相互作用对倾斜椭圆射流(主、次平面倾角均为30°)夹带的积极影响。实验在宽高比(AR)为2,雷诺数约为3000的条件下进行。采用时间分辨层析粒子图像测速(Tomo-PIV)和三维拉格朗日粒子跟踪(3D LPT)测量技术详细捕捉了流体动力学。利用三维LPT测量的高精度轨迹增强了Tomo-PIV获得的欧拉速度场数据集,提高了速度场重建的精度。统计分析表明,与非倾斜椭圆射流相比,倾斜椭圆射流表现出更大的质量夹带特性和更高的动量通量。功率谱密度(psd)和时域谱固有正交分解(td-SPOD)结果表明,在主平面斜a喷嘴中,前后涡环的主导频率均为St = 0.28,表明30°斜a射流中的涡配对和合并可能是一个周期性过程。当涡旋在Y/De≈3.5处合并后,完成了第一次轴向转换,这表明与非倾斜情况相比,主平面倾斜a椭圆射流的轴向转换受到抑制。而对于小平面斜b射流,前涡环和后涡环的主导频率分别为St = 0.28和St = 0.61。在某些情况下,对应于SPOD模态(3,4)的两个连续大尺度涡环下游不合并;相反,它们各自独立发展,最终各自瓦解。在换轴平面(Y/De = 2.5),在两个倾斜喷嘴内涡环的合并和换轴过程中,都会产生大量的流向涡结构。这种现象大大增加了平均夹带速率,进一步增强了倾斜椭圆射流的混合特性。图形抽象
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来源期刊
Experiments in Fluids
Experiments in Fluids 工程技术-工程:机械
CiteScore
5.10
自引率
12.50%
发文量
157
审稿时长
3.8 months
期刊介绍: Experiments in Fluids examines the advancement, extension, and improvement of new techniques of flow measurement. The journal also publishes contributions that employ existing experimental techniques to gain an understanding of the underlying flow physics in the areas of turbulence, aerodynamics, hydrodynamics, convective heat transfer, combustion, turbomachinery, multi-phase flows, and chemical, biological and geological flows. In addition, readers will find papers that report on investigations combining experimental and analytical/numerical approaches.
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