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Effect of Jet Inclination Angle and Hole Exit Shape on Vortical Flow Structures in Low-Reynolds Number Jet in Cross-Flow

机译:喷射倾斜角和孔出口形状对交叉流动低雷诺数射流涡流结构的影响

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摘要

Numerical studies have been performed to visualize vortical flow structures emerged from jet cross-flow interactions. A single square jet issuing perpendicularly into a cross-flow was simulated first, followed by two additional scenarios, that is, inclined square jet at angles of 30° and 60° and round and elliptic jets at an angle of 90°, respectively. The simulation considers a jet to cross-flow velocity ratio of 2.5 and a Reynolds number of 225, based on the free-stream flow quantities and the jet exit width in case of square jet or minor axis length in case of elliptic jet. For the single square jet, the vortical flow structures simulated are in good qualitative agreement with the findings by other researchers. Further analysis reveals that the jet penetrates deeper into the cross-flow field for the normal jet, and the decrease of the jet inclination angle weakens the cross-flow entrainment in the near-wake region. For both noncircular and circular jet hole shapes, the flow field in the vicinity of the jet exit has been dominated by large-scale dynamic flow structures and it was found that the elliptic jet hole geometry has maximum “lifted-off” effect among three hole configurations studied. This finding is also in good qualitative agreement with existing experimental observations.
机译:已经进行了数值研究以可视化从喷射交叉流动相互作用出现的涡流流动结构。首先模拟垂直于横流的单个方形射流,然后进行两种额外的场景,即在30°和60°的角度为30°和60°的角度,分别为90°的圆形射流。基于在椭圆射流的方形射流或短轴长度的情况下,基于自由流流量和射流出口宽度,模拟将射流与2.5和雷诺数为225的逆流速度比。对于单方面喷射,模拟的涡流结构与其他研究人员的调查结果良好。进一步的分析揭示了喷射渗透到正常射流的横流场中,并且射流倾斜角的降低削弱了近唤醒区域中的横流夹带。对于非圆形和圆形喷射孔形状,喷射出口附近的流场已经由大规模的动态流动结构主导,发现椭圆射流几何形状在三个孔中最大“抬起”效果。研究研究。这种发现也与现有的实验观察结果良好。

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