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Transverse jet mixing characteristics

机译:横向喷射混合特性

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This experimental study explores and quantifies mixing characteristics associated with a gaseous round jet injected perpendicularly into cross-flow for a range of flow and injection conditions. The study utilizes acetone planar laser-induced fluorescence imaging to determine mixing metrics in both centreplane and cross-sectional planes of the jet, for a range of jet-to-cross-flow momentum flux ratios (2 <= J <= 41), density ratios (0.35 <= S <= 1.0) and injector configurations (flush nozzle, flush pipe and elevated nozzle), all at a fixed jet Reynolds number of 1900. For the majority of conditions explored, there is a direct correspondence between the nature of the jet's upstream shear layer instabilities and structure, as documented in detail in Getsinger et al. (J. Fluid Mech., vol. 760, 2014, pp. 342-367), and the jet's mixing characteristics, consistent with diffusion-dominated processes, but with a few notable exceptions. When quantified as a function of distance along the jet trajectory, mixing metrics for jets in cross-flow with an absolutely unstable upstream shear layer and relatively symmetric counter-rotating vortex pair cross-sectional structure tend to show better local molecular mixing than for jets with convectively unstable upstream shear layers and generally asymmetric cross-sectional structures. Yet the spatial evolution of mixing with downstream distance can he greater for a few specific convectively unstable conditions, apparently associated with the initiation and nature of shear layer rollup as a trigger for improved mixing. A notable exception to these trends concerns conditions where the equidensity jet in cross-flow has an upstream shear layer that is already absolutely unstable, and the jet density is then reduced in comparison with that of the cross-flow. Here, density ratios below unity tend to mix less well than for equidensity conditions, demonstrated to result from differences in the nature of higher-density cross-flow entrainment into lower-density shear layer vortices.
机译:这项实验研究探索并量化了在一定范围内的流动和注入条件下,垂直于错流喷射的气态圆形射流的混合特性。这项研究利用丙酮平面激光诱导的荧光成像技术来确定一系列射流与横流动量通量之比(2 <= J <= 41)时,射流的中心平面和横截面的混合指标,密度比(0.35 <= S <= 1.0)和喷射器配置(冲洗喷嘴,冲洗管和升高的喷嘴),都是在固定的1900雷诺数下进行的。对于大多数探索的条件,性质之间存在直接对应喷气机上游剪切层的不稳定性和结构,详见Getsinger等人。 (J. Fluid Mech。,第760卷,2014年,第342-367页),以及射流的混合特性,与扩散控制的过程一致,但有一些值得注意的例外。当量化为沿着射流轨迹的距离的函数时,具有绝对不稳定的上游剪切层和相对对称的反向旋转涡流对横截面结构的错流射流的混合度量往往显示出比具有以下特征的射流更好的局部分子混合:对流不稳定的上游剪切层和通常不对称的横截面结构。然而,在一些特定的对流不稳定条件下,与下游距离混合的空间演化可能会更大,这显然与剪切层上卷的开始和性质相关,从而可以改善混合。这些趋势的显着例外涉及条件,其中横流中的均流射流具有已经绝对不稳定的上游剪切层,然后与横流相比,射流密度降低了。在这里,低于1的密度比往往比均匀条件下混合得不好,这被证明是由高密度错流夹带到低密度剪切层涡旋中的性质不同引起的。

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