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Large eddy simulation of turbulent channel flow using differential equation wall model

机译:基于微分方程壁模型的湍流通道大涡模拟

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A large eddy simulation (LES) of a plane turbulent channel flow is performed at a Reynolds number Re? = 590 based on the channel half width, ? and wall shear velocity, u? by approximating the near wall region using differential equation wall model (DEWM). The simulation is performed in a computational domain of 2? ? x 2 ? x?? ? . The computational domain is discretized by staggered grid system with 32 x 30 x 32 grid points. In this domain the governing equations of LES are discretized spatially by second order finite difference formulation, and for temporal discretization the third order low-storage Runge-Kutta method is used. Essential turbulence statistics of the computed flow field based on this LES approach are calculated and compared with the available Direct Numerical Simulation (DNS) and LES data where no wall model was used. Comparing the results throughout the calculation domain we have found that the LES results based on DEWM show closer agreement with the DNS data, especially at the near wall region. That is, the LES approach based on DEWM can capture the effects of near wall structures more accurately. Flow structures in the computed flow field in the 3D turbulent channel have also been discussed and compared with LES data using no wall model.
机译:平面湍流通道的大涡模拟(LES)在雷诺数Re?下进行。 = 590基于通道半宽度,?和壁面剪切速度,u?通过使用微分方程墙模型(DEWM)逼近近壁区域。模拟在2?的计算域中执行。 ? 2倍X?? ? 。计算域由具有32 x 30 x 32网格点的交错网格系统离散化。在这个领域,LES的控制方程通过二阶有限差分公式在空间上离散,对于时间离散,使用三阶低存储Runge-Kutta方法。计算基于此LES方法的计算流场的基本湍流统计量,并将其与不使用任何壁模型的可用直接数值模拟(DNS)和LES数据进行比较。在整个计算域中比较结果,我们发现基于DEWM的LES结果与DNS数据显示出更紧密的一致性,尤其是在近壁区域。也就是说,基于DEWM的LES方法可以更准确地捕获近墙结构的影响。还讨论了在3D湍流通道中计算的流场中的流动结构,并使用无壁模型将其与LES数据进行了比较。

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