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首页> 外文期刊>International Journal of Naval Architecture and Ocean Engineering >Reynolds and froude number effect on the flow past an interface-piercing circular cylinder
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Reynolds and froude number effect on the flow past an interface-piercing circular cylinder

机译:雷诺数和弗洛德数对流经穿刺圆柱体的流量的影响

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ABSTRACT The two-phase turbulent flow past an interface-piercing circular cylinder is studied using a high-fidelity orthogonal curvilinear grid solver with a Lagrangian dynamic subgrid-scale model for large-eddy simulation and a coupled level set and volume of fluid method for air-water interface tracking. The simulations cover the sub-critical and critical and post critical regimes of the Reynolds and sub and super-critical Froude numbers in order to investigate the effect of both dimensionless parameters on the flow. Significant changes in flow features near the air-water interface were observed as the Reynolds number was increased from the sub-critical to the critical regime. The interface makes the separation point near the interface much delayed for all Reynolds numbers. The separation region at intermediate depths is remarkably reduced for the critical Reynolds number regime. The deep flow resembles the single-phase turbulent flow past a circular cylinder, but includes the effect of the free-surface and the limited span length for sub-critical Reynolds numbers. At different Froude numbers, the air-water interface exhibits significantly changed structures, including breaking bow waves with splashes and bubbles at high Froude numbers. Instantaneous and mean flow features such as interface structures, vortex shedding, Reynolds stresses, and vorticity transport are also analyzed. The results are compared with reference experimental data available in the literature. The deep flow is also compared with the single-phase turbulent flow past a circular cylinder in the similar ranges of Reynolds numbers. Discussion is provided concerning the limitations of the current simulations and available experimental data along with future research.
机译:摘要使用高保真正交曲线网格求解器和拉格朗日动态子网格规模模型进行大涡流仿真,并采用耦合水平集和空气体积耦合方法研究流经穿刺圆柱体的两相湍流-水界面跟踪。为了研究这两个无量纲参数对流动的影响,模拟涵盖了雷诺兹的亚临界,临界和后临界状态以及亚临界和超临界弗洛德数。随着雷诺数从次临界状态增加到临界状态,在空气-水界面附近的流动特征发生了显着变化。对于所有雷诺数,该接口会使接口附近的分离点延迟很多。对于临界雷诺数制度,中间深度处的分离区域显着减小。深流类似于经过圆柱体的单相湍流,但是包括自由表面的作用和亚临界雷诺数的有限跨度。在不同的弗洛德数下,空气-水界面的结构发生了显着变化,包括在高弗洛德数下破裂带有飞溅和气泡的弓形波。还分析了瞬时和平均流动特征,例如界面结构,涡旋脱落,雷诺应力和涡旋传输。将结果与文献中提供的参考实验数据进行比较。在相似的雷诺数范围内,还将深流与经过圆柱体的单相湍流进行了比较。讨论了当前模拟的局限性以及可用的实验数据以及未来的研究。

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