空间发展边界层的大涡模拟

Xiaohua Wu, K. Squires, T. Lund
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引用次数: 11

摘要

描述了一种用于模拟空间发展边界层的三维、随时间变化的湍流入流条件的生成方法。假设边界层自保存,定义一个准齐次坐标,沿此坐标沿流不均匀性最小化(Spalart 1988)。利用这种准齐次坐标,将速度分解为平均部分和周期部分,在每个时间步长在流内边界重新引入计算域出口边界附近位置的速度场。在动量厚度雷诺数范围为1470 ~ 1700的平板边界层大涡模拟中,对该方法进行了验证。采用Germano等人(1991)的动态涡流黏度模型模拟亚网格尺度应力。模拟结果表明,使用本方法可以再现空间发展的湍流边界层的基本特征,而不需要长时间和计算昂贵的层流-湍流过渡区。边界层特性如表面摩擦和形状因子以及平均速度分布和湍流强度与实验测量和直接数值模拟的结果吻合得很好。本文还介绍了该方法在空间发展复杂湍流边界层计算中的应用。
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Large Eddy Simulation of a Spatially-Developing Boundary Layer
A method for generation of a three-dimensional, time-dependent turbulent inflow condition for simulation of spatially-developing boundary layers is described. Assuming self-preservation of the boundary layer, a quasi-homogeneous coordinate is defined along which streamwise inhomogeneity is minimized (Spalart 1988). Using this quasi-homogeneous coordinate and decomposition of the velocity into a mean and periodic part, the velocity field at a location near the exit boundary of the computational domain is re-introduced at the in- flow boundary at each time step. The method was tested using large eddy simulations of a flat-plate boundary layer for momentum thickness Reynolds numbers ranging from 1470 to 1700. Subgrid scale stresses were modeled using the dynamic eddy viscosity model of Germano et al. (1991). Simulation results demonstrate that the essential features of spatially-developing turbulent boundary layers are reproduced using the present approach without the need for a prolonged and computationally expensive laminar-turbulent transition region. Boundary layer properties such as skin friction and shape factor as well as mean velocity profiles and turbulence intensities are in good agreement with experimental measurements and results from direct numerical simulation. Application of the method for calculation of spatially-developing complex turbulent boundary layers is also described.
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