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Large scale structure and mixing in a sonic transverse jet injected into a supersonic crossflow.

机译:大型结构并在注入超声速横流的声波横向射流中混合。

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The large scale structure and mixing characteristics of the flowfield surrounding a single, underexpanded, sonic, transverse jet injected into a Mach 1.6 crossflow were experimentally studied. The flowfield was investigated at three distinct sets of flow conditions corresponding to a jet-to-crossflow momentum flux ratio of 1.2, 1.7, and 2.2. Planar laser-induced fluorescence from acetone molecules and planar Mie scattering from condensed ethanol droplets were used to obtain spatially and temporally resolved flowfield visualizations in various side, end, and top view image planes. Statistical processing of the image ensembles produced mean and standard deviation images, two-dimensional spatial autocovariance fields representing the characteristics of the dominant turbulent structures, and probability density functions representing the instantaneous state of scalar mixing in the flowfield.; Time-averaged descriptions of the mixing characteristics of this transverse jet flowfield were shown to be inaccurate. Intermittent large scale structures of various sizes, shapes, and orientations strongly influence the distribution of the jet fluid and the crossflow fluid. Relatively high probabilities of unmixed fluid (whether jet or crossflow) persist in many of the mixing regions between the jet and crossflow. The most significant instantaneous mixing in this flowfield seems to occur in the center of wake region slightly below the jet centerline. A counter-rotating streamwise vortex pair in the jet cross section plays an important role in the scalar mixing processes, as it transports jet fluid down towards the wake and entrains crossflow fluid from below up into the jet. The streamwise vortex pair initially develops in an asymmetric and undulating manner, but gradually becomes more symmetric farther downstream of the Mach disk. A relatively large portion of the total jet fluid bypasses the Mach disk through the upstream edge of the barrel shock, thereby retaining a significant fraction of its momentum. This relatively high momentum jet fluid penetrates deeply into the crossflow, contributes to the formation of the largest turbulent structures, and affects the evolution of the streamwise vortex pair.
机译:通过实验研究了注入到Mach 1.6错流中的单个,未充分扩展的声波横向射流周围的流场的大规模结构和混合特性。在三组不同的流动条件下研究了流场,分别对应于射流与横流的动量通量比为1.2、1.7和2.2。来自丙酮分子的平面激光诱导的荧光和来自浓缩乙醇滴的平面Mie散射被用于在各个侧面,端面和顶视图图像平面中获得时空分辨的流场可视化效果。图像集合的统计处理产生了均值和标准差图像,代表了主要湍流结构特征的二维空间自协方差场,以及代表了流场中标量混合瞬时状态的概率密度函数。该横向射流流场的混合特性的时间平均描述被证明是不准确的。各种大小,形状和方向的间歇性大型结构会强烈影响喷射流体和错流流体的分布。在射流和横流之间的许多混合区域中,存在较高的未混合流体(无论是射流还是横流)的可能性。在此流场中,最明显的瞬时混合似乎发生在尾流区域的中心,该区域略低于射流中心线。射流横截面中的反向旋转涡流对在标量混合过程中起重要作用,因为它将射流流体向下流向尾流,并从下方将夹流流体带入射流。涡流对最初以不对称和起伏的方式发展,但在马赫盘的下游逐渐变得更加对称。总射流的相对较大部分通过机筒冲击的上游边缘绕过马赫盘,从而保留了很大一部分动量。这种相对较高动量的射流流体深深地渗透到错流中,有助于形成最大的湍流结构,并影响流向涡流对的演化。

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