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Large-eddy simulation of accelerating boundary layers

机译:加速边界层的大涡模拟

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Large-eddy simulation of flat-plate boundary layers in favorable pressure gradients (FPG) are performed for two different acceleration parameters. The high-acceleration case is in good agreement with the experimental data by Fernholz and Warnack. Substantial reduction in turbulent kinetic energy, strong decorrelation of u and v fluctuation, and a reduction of the bursting frequency indicate that the accelerated boundary layer is in a laminar-like state when the pressure-gradient parameter K exceeds a threshold value. Downstream of this region, the boundary layer has a fast re-transition to turbulence: it seems due to the turbulent structures present in the outer part of the boundary layer. In the low K case, the boundary layer does not depart significantly from equilibrium.
机译:对两个不同的加速度参数进行良好的压力梯度(FPG)的平板边界层的大涡流模拟。高速加速案例与Fernholz和Warnack的实验数据吻合良好。湍流动能的大幅度降低,U和V波动的强脱节,以及爆破频率的减小表明,当压力梯度参数k超过阈值时,加速边界层处于层状状态。在该区域的下游,边界层具有快速重新过渡到湍流:似乎是由于边界层的外部中存在的湍流结构。在低k个情况下,边界层不会显着地偏离均衡。

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