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Evolution of three-dimensional temporally evolving plane mixing layers under strong vortex disturbances

机译:强涡旋扰动下三维时间演化平面混合层的演化

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The evolution of three-dimensional temporally evolving plane mixing layers under strong vortex disturbances is investigated by DNS method. The convective Mach number and the Reynolds number used is set to be 0.8 and 200. The isentropic vortex is chosen as the model for vortex disturbances. Three different directions of the vortex axis (streamwise, spanwise, and normal directions) are considered in the simulations. For comparison, the computation with linear unstable oblique waves as disturbances is also executed. The results show that in the case of the streamwise vortex disturbance, significant increase in vorticity thickness can be found only in the early stage of development. In the case of the normal vortex disturbance, a high growth rate of the plane mixing layer is kept all the time, while in the linear wave case saturation occurs in the later stage of the simulation and the vorticity thickness stops increasing further. In the case of the spanwise vortex disturbance, the flow is quite quiet and the vorticity thickness attains the lowest growth rate.
机译:利用DNS方法研究了强涡旋扰动下三维时间演化平面混合层的演化。对流马赫数和雷诺数分别设置为0.8和200。选择等熵涡流作为涡流扰动的模型。在模拟中考虑了涡流轴的三个不同方向(沿流向,跨度和法线方向)。为了进行比较,还执行了以线性不稳定斜波为扰动的计算。结果表明,在沿流涡旋扰动的情况下,仅在发展的早期阶段才能发现涡旋厚度的显着增加。在正常涡旋扰动的情况下,一直保持平面混合层的高生长速率,而在线性波情况下,在模拟的后期出现饱和,并且涡旋厚度不再进一步增加。在翼展方向涡旋扰动的情况下,流动非常安静,涡旋厚度达到最低的增长率。

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