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LARGE EDDY SIMULATION OF TURBULENT HEAT TRANSFER AROUND A CIRCULAR CYLINDER IN CROSSFLOW

机译:绕流圆柱绕湍流传热的大涡模拟

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Large eddy simulation has been carried out of turbulent flow and heat transfer around a circular cylinder in crossflow at three subcritical Reynolds numbers (Re = 3,900, 10,000, 18,900) where the flow and heat transfer characteristics change rapidly with the Reynolds number. The computations were carried out using a second-order-accurate finite-volume Navier-Stokes solver that permits use of arbitrary unstructured meshes. A fully implicit, non-iterative fractional-step method was employed to advance the solution in time. The subgrid-scale (SGS) turbulent stresses and heat fluxes were modeled using the dynamic Smagorinsky model. The LES predictions were found to be in good agreement with the experimental data of Hajime and Igarashi (2004). The salient features of turbulent heat transfer in subcritical regime such as the laminar thermal boundary layer and the rapid increase with Reynolds number both in the mean and the r.m.s. Nusselt number in the separated region are closely reproduced by the predictions. The numerical results confirmed that the heat transfer characteristics are closely correlated with the structural change in the underlying flow with the Reynolds number.
机译:在三个亚临界雷诺数(Re = 3,900,10,000,18,900)下,在横流中绕圆柱体的湍流和传热进行了大涡模拟,其中,流动和传热特性随雷诺数快速变化。使用允许使用任意非结构化网格的二阶精确有限体积Navier-Stokes求解器进行了计算。采用完全隐式,非迭代分数步法来及时解决问题。使用动态Smagorinsky模型对亚网格规模(SGS)的湍流应力和热通量进行建模。发现LES预测与Hajime和Igarashi(2004)的实验数据非常吻合。亚临界状态下湍流传热的显着特征,例如层流热边界层,以及均值和均方根值均随雷诺数的增加而迅速增加。通过预测可以精确地复制分离区域中的Nusselt数。数值结果证实,传热特性与雷诺数与下层流动的结构变化密切相关。

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