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Direct simulation of turbulent swept flow over a wire in a channel

机译:直接模拟通道中导线上的湍流扫掠流

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Turbulent swept flow over a cylindrical wire placed on a wall of a channel is investigated usingidirect numerical simulations: This geometry is a model of the flow through the, wire-wrapped fuel pins, the heat exchanger, typical of many nuclear reactor designs. Mean flow along and across the wire axis is :imposed, leading to the formation of separated flow regions. The Reynolds number based on the bulk yelocity along' the wire axis direction and the channel half height is 5400 and four cases are simulated with different flowrates across the wire. This configuration is topologically similar to backward-facing steps or slots with swept flow; except that the dominant flow is along the obstacle axis in the present study and the crossflow is smaller than the axial flow, i.e. the sweep angle, is large. Mean 'velocities, turbulence statistics, wall shear stress and instantaneous flow structures are investigated. Particular attention is devoted to the statistics of the shear stress on the walls of the channel and the wire in the. recirculation zone. The Slow around the mean reattachment region, at the termination of the recirculating bubble,, does not exhibit, the typical decay of the mean shear stress observed in classical ,backward-facing step flows owing to the presence of a strong axial flow. The evolution of the mean wall shear stress angle after reattachment indicates that the flow recovers. towards equilibrium at a rather slow rate, which decreases with sweep, angle. Finally,, the database is analysed to estimate resolution, requirements, in particular around the recirculation zones, for large-eddy-simulations. This has implications in more complete geometrical models of a wire-wrapped assembly, involving hundreds of fuel, pins, where. only turbulence modelling can be afforded, computationally.
机译:使用直接数值模拟研究了放置在通道壁上的圆柱丝上的湍流掠流:此几何形状是通过许多燃料电池反应堆设计中典型的绕线燃料棒,热交换器的流动的模型。沿着和跨过导线轴线的平均流量被施加,导致形成分离的流动区域。基于沿线材轴线方向的体孔率和通道半高的雷诺数为5400,并模拟了四种情况,其中线材的流速不同。这种配置在拓扑上类似于后向步骤或带有扫掠流的槽。除了主要的流动是沿着障碍物轴,在本研究中,交叉流小于轴向流,即后掠角大。研究了平均速度,湍流统计,壁面剪应力和瞬时流动结构。特别注意的是通道壁和通道中壁上的剪应力的统计。回流区。在循环气泡终止时,平均重新附着区域周围的缓慢现象并没有表现出由于存在强大的轴向流,在经典的向后步骤流动中观察到的平均剪切应力的典型衰减。重新安装后,平均壁面剪应力角的变化表明流动得以恢复。以相当慢的速度向平衡方向移动,该速度随掠角和角度的减小而减小。最后,对数据库进行分析以估计分辨率,要求,尤其是在大涡流模拟的再循环区域附近。这对绕线组件的更完整的几何模型有影响,其中涉及数百个燃料,销钉。在计算上只能提供湍流建模。

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