首页> 外文会议>Second Asia-Pacific International Conference on Numerical Methods in Engineering 2006 (ICOME 2006) >Free Surface Flow Past a Piercing Circular Cylinder at High Froude Numbers
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Free Surface Flow Past a Piercing Circular Cylinder at High Froude Numbers

机译:自由表面流以高弗劳德数通过穿孔圆柱体

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Flows past a free surface piercing cylinder are studied numerically by large eddy simulation (LES) at Froude numbers up to FrD=2.0 and Reynolds numbers up to ReD=1.10^5. A two-phase FCT-VOF method is employed to simulate the air-water interface. The effects of the free surface on vortex structure and Reynolds stress in the near wake are investigated. The loadings on the cylinder at various Reynolds and Froude numbers are also studied. Computation results show the free surface inhibits the vortex generation in the near wake, and this effect is stronger at higher Froude numbers. At a relatively lower Froude number, FrD=0.8, a vortex street characterized by a dominant mode of StD~0.23 is observed in the area away from the free surface, whereas no regular vortex shedding is found throughout the wake at a higher Froude number (FrD=2.0). It is also shown that the strong three dimensionality in the near wake at higher Froude numbers affects the force distribution dramatically along the cylinder, whereas variation in the Reynolds number has no significant effect. At FrD=2.0, in the region well below the free surface, there is a huge increase of both the mean drag and rms lift.
机译:通过大涡模拟(LES)在Froude数最大为FrD = 2.0的情况下和Reynolds数最大为ReD = 1.10 ^ 5的情况下,对通过自由表面穿孔缸的流动进行了数值研究。采用两相FCT-VOF方法模拟空气-水界面。研究了自由表面对近尾流中涡旋结构和雷诺应力的影响。还研究了不同雷诺数和弗洛德数下圆柱体的载荷。计算结果表明,自由表面在近尾时抑制了涡流的产生,并且在较高的弗洛德数下,这种作用更强。在相对较低的弗洛德数FrD = 0.8处,在远离自由表面的区域中观察到以StD〜0.23的主导模式为特征的涡街,而在较高的弗洛德数下,整个尾波均未发现规则的涡流脱落( FrD = 2.0)。还表明,在较高的弗劳德数下,近尾处的强三维度极大地影响了沿圆柱的力分布,而雷诺数的变化没有显着影响。在FrD = 2.0时,在自由表面以下的区域中,平均阻力和均方根升幅都大大增加。

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