Experimental Investigation of a High Velocity Gaseous Jet Injection Into an Oscillating Crossflow

Jinkwan Song, J. Wilson, J. Lee
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Abstract

This paper presents the experimental results of a gaseous jet injected into an oscillating-air crossflow. The jet to crossflow momentum flux ratios are chosen as 19, 30 and 58, and the mean air crossflow velocities are chosen as 10m/s, 25 m/s, and 60 m/s. The crossflow is modulated at frequencies up to 280 Hz with a maximum crossflow velocity fluctuation of 30% of its mean velocity. Acetone planar laser-induced fluorescence is used to record the instantaneous jet concentration field. Three distinct regions are observed near the injection location (x/d < 18); the jet core, the fast bending zone, and the fully developed plume zone. The location of the end of potential core can be determined primarily by the momentum flux ratio. Based on observations of these three regions, a set of correlations for the trajectory of maximum jet concentration is proposed for the potential core region and for the fully developed plume zone. The potential core responds quasi-steadily to the crossflow oscillation and the fluctuation of penetration of the potential core zone linearly increases with respect to the crossflow velocity fluctuation level. The jet penetration under oscillating crossflow is slightly lower than that under steady crossflow, especially when the mean crossflow velocity is low (10–25 m/s). However, the differences of trajectories between the oscillating and the steady crossflow cases become almost negligible as the mean crossflow velocity increases further. The axial decay of jet concentration under oscillating crossflow occurs at faster rate than that under steady crossflow, indicating that the oscillating air crossflow enhances the mixing between the jet and the crossflow. The vertical jet concentration profile at different axial location confirms that the main effect of crossflow modulation is enhanced mixing of jet with crossflow. However, no noticeable effect of modulation frequency of crossflow on the jet penetration is found.
高速气体射流注入振荡横流的实验研究
本文介绍了气体射流注入振荡空气横流的实验结果。射流与横流动量通量比分别为19、30和58,平均空气横流速度分别为10m/s、25m /s和60m /s。横流的调制频率高达280 Hz,横流的最大速度波动为其平均速度的30%。利用丙酮平面激光诱导荧光记录瞬时射流浓度场。在注射部位附近观察到三个明显的区域(x/d < 18);射流核、快速弯曲带和充分发育的羽流带。势核末端的位置主要由动量通量比确定。根据这三个区域的观测结果,提出了潜在核心区和完全发育的羽流区最大射流浓度轨迹的一组相关关系。势核对横流振荡的响应准稳定,势核区的穿透波动随横流速度波动程度线性增加。振荡横流条件下射流侵彻略低于定常横流条件下,特别是平均横流速度较低时(10 ~ 25 m/s)。然而,随着平均横流速度的进一步增大,振荡和定常横流情况下的轨迹差异几乎可以忽略不计。振荡横流条件下射流浓度的轴向衰减速度比定常横流条件下更快,说明振荡空气横流增强了射流与横流的混合。不同轴向位置的垂直射流浓度曲线证实了横流调制的主要效果是增强了射流与横流的混合。而横流调制频率对射流侵彻的影响不明显。
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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