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High Performance Computing of the flow past a circular cylinder at critical and supercritical Reynolds numbers

机译:在临界和超临界雷诺数的圆柱体上的高性能计算流过圆柱体

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It is well known that the flow past a circular cylinder at critical Reynolds number combines flow separation, turbulence transition, reattachment of the flow and further turbulent separation of the boundary layer. In the critical regime, the transition to turbulence in the boundary layer causes the delaying of the separation point and, an important reduction of the drag force on the cylinder surface known as the Drag Crisis. In this paper advanced turbulence simulations at Reynolds numbers in the range of 1.4 x 10~5-8.5 x 10~5 will be carried out by means of large-eddy simulations. Numerical simulations using unstructured grids up to 70 million of control volumes have been performed on Marenostrum Supercomputer. One of the major outcomes is shedding some light on the shear layer instabilities mechanisms and their role on the drag crisis phenomena.
机译:众所周知,通过临界雷诺数的圆柱体的流动结合了流动分离,湍流转变,流动的湍流和边界层的进一步湍流分离。在临界制度中,边界层中的湍流过渡导致分离点的延迟,并且在称为阻力危机的汽缸表面上的拖曳力的重要减小。在本文中,雷诺数的高级湍流模拟在1.4×10〜5-8.5×10〜5的范围内将通过大涡模拟进行。在Marenostrum超级计算机上进行了使用非结构化网格的数值模拟高达7000万辆的控制体积。其中一个主要结果是在剪切层稳定性机制上脱离一些光线及其对拖累危机现象的作用。

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