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A numerical study on the eddy structures of impinging jets excited at the inlet

机译:入口处激发射流涡流结构的数值研究

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Three-dimensional eddy structures arising in plane and round impinging jets excited at the nozzle inlet were investigated numerically by direct numerical simulation and large eddy simulation. Special attention is focused on how spanwise or azimuthal disturbances imposed at the inlet velocity affect the eddy structures in the transition process. In this respect, three spatial wavelength of λ/πD = 1/3, 1/4 and 1/6, where D is the nozzle width or the diameter, were tested in this study. It was found that the round jet showed definite instability at λ/πD = 1/6 while the plane jet showed almost equivalent sensitivity to all modes tested here. As regards the eddy structures in the stagnation region, elongated twin vortices along the impinging plate of the plane jet were reproduced and the number of pairs was found to agree exactly with the span wise wave number imposed at the inlet. In contrast to the plane jet, no organized structures were observed in the stagnation region of the round jet.
机译:通过直接数值模拟和大涡模拟,对在喷嘴进口处激发的平面和圆形冲击射流中产生的三维涡结构进行了数值研究。特别注意的是在过渡过程中以入口速度施加的跨度或方位扰动如何影响涡流结构。在这方面,在本研究中测试了三个空间波长为λ/πD= 1 / 3、1 / 4和1/6,其中D为喷嘴宽度或直径。发现圆形射流在λ/πD= 1/6时表现出一定的不稳定性,而平面射流对此处测试的所有模式都表现出几乎相同的灵敏度。至于停滞区的涡流结构,沿平面射流撞击板的细长双涡旋被复制,对数与进口处的展向波数精确一致。与平面射流相反,在圆形射流的停滞区域没有观察到有组织的结构。

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