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Direct numerical simulation of round turbulent jets in crossflow

机译:横流中圆形湍流射流的直接数值模拟

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Direct numerical simulation is used to study a round turbulent jet in a laminar crossflow. The ratio of bulk jet velocity to free-stream crossflow velocity is 5.7 and the Reynolds number based on the bulk jet velocity and the jet exit diameter is 5000. The mean velocity and turbulent intensities from the simulations are compared to data from the experiments by Su & Mungal (2004) and good agreement is observed. Additional quantities, not available from experiments, are presented. Turbulent kinetic energy budgets are computed for this flow. Examination of the budgets shows that the near field is far from a state of turbulent equilibrium - especially along the jet edges. Also - in the near field - peak kinetic energy production is observed close to the leading edge, while peak dissipation is observed toward the trailing edge of the jet. The results are used to comment upon the difficulty involved in predicting this flow using RANS computations. There exist regions in this flow where the pressure transport term, neglected by some models and poorly modelled by others, is significant. And past the jet exit, the flow is not close to established canonical flows on which most models appear to be based.
机译:直接数值模拟用于研究层流错流中的圆形湍流射流。整体射流速度与自由流横流速度之比为5.7,基于整体射流速度和射流出口直径的雷诺数为5000。将模拟所得的平均速度和湍流强度与Su实验所得的数据进行比较&Mungal(2004)和良好的协议被观察到。提出了无法从实验中获得的其他数量。为此流动计算了湍动能预算。预算检查表明,近场远非湍流平衡状态,尤其是沿射流边缘。另外-在近场中-在靠近前缘处观察到峰值动能产生,而在射流后缘处观察到峰值耗散。结果用于说明使用RANS计算预测此流量所涉及的困难。在该流中存在一些区域,其中某些模型所忽略而其他模型所欠佳的压力传输项很重要。并且经过射流出口后,流量并不接近大多数模型似乎基于的既定规范流量。

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