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Numerical Simulation of a Rectangular Jet by the Vortex in Cell Method

机译:矩形涡流的单元法涡旋数值模拟

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This study is concerned with the large eddy simulation (LES) for a jet issuing from a rectangular nozzle. The Vortex in Cell (VIC) method, of which computational accuracy was heightened by the authors in a prior study, is used for the simulation. The aspect ratio of the nozzle cross-section is 15, and the Reynolds number based on the shorter side length of the nozzle is 6700. The simulation highlights that the turbulence statistics, such as the mean velocity and the turbulence intensity, are favorably compared with the corresponding experimental results. The appearance of large-scale eddies due to the instability of the shear layer originating from the nozzle edges, the collapse of the eddies, and the subsequent development of the turbulent flow are also successfully grasped by the simulation. These demonstrate that the employed VIC method is indeed applicable to jet simulation.
机译:这项研究与从矩形喷嘴喷出的大涡模拟(LES)有关。仿真中使用了作者在以前的研究中提高了计算精度的单元中涡旋(VIC)方法。喷嘴横截面的长宽比为15,基于喷嘴较短边长的雷诺数为6700。仿真结果表明,与平均速度和湍流强度等湍流统计数据相比,它具有优势。相应的实验结果。通过模拟还成功地把握了由于来自喷嘴边缘的剪切层的不稳定性,涡流的坍塌以及湍流的后续发展而导致的大涡流的出现。这些证明所采用的VIC方法确实适用于射流模拟。

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