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On the Convection Velocity of Wall-Bounded Turbulence Resolved by ZDES Mode III at Re_θ= 13000

机译:ZDES模式III在RE_θ= 13000的对流速度

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1 Short Discussion of the Need and Options for Wall-Modelled Large Eddy Simulation in Applied Aerodynamics In applied aerodynamics, the increasing demand for the prediction of phenomena such as mild flow separations, strongly out of equilibrium boundary layers, aeroa-coustics or unsteady loading may require a more detailed and universal description than the mean values provided by Reynolds Averaged Navier-Stokes models, motivating turbulence-resolving approaches of wall-bounded flows. However, in high Reynolds number attached turbulent boundary layers in most aerospace applications (Reτ ≈ 10~4 - 10~5), the numerical cost of Direct Numerical Simulation, and even of Wall-Resolved Large Eddy Simulation, is prohibitive because of the lack of scale separation in the near-wall region. Introducing wall models and resolving the outer layer dynamics, the number of grid points for Wall-Modelled Large Eddy Simulation is approximately proportional to the square root of the number of points for DNS (see [61), making WMLES affordable in applied aerodynamics at high Reynolds numbers.
机译:的需要,并且对于选项1简短讨论墙建模的大涡模拟在应用空气动力学在施加空气动力学,为的现象的预测的需求不断增加,例如温和的边界层分离,强烈出的平衡边界层,aeroa-coustics或不稳定的负载可需要的更详细的和普遍的描述不是由雷诺数提供的平均取平均值的Navier-Stokes模型,激励有界壁的流动的湍流的解决途径。然而,在高雷诺数附着在大多数航空航天应用湍流边界层(Reτ≈10〜4 - 10〜5),直接数值模拟的数值成本,甚至墙分辨大涡模拟,是因为缺乏望而却步在近壁区标分离。导入壁模型和解决外层动力学,对于壁挂式仿照大涡模拟网格点的数量是大致成比例的DNS点的数量的平方根(见[61),使得WMLES实惠在高施加空气动力学雷诺数。

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