A Parametric Kinetic Solver for Simulating Boundary-Dominated Turbulent Flow Phenomena

Mengyun Liu, Xiaopei Liu
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Abstract

Boundary layer flow plays a very important role in shaping the entire flow feature near and behind obstacles inside fluids. Thus, boundary treatment methods are crucial for a physically consistent fluid simulation, especially when turbulence occurs at a high Reynolds number, in which accurately handling thin boundary layer becomes quite challenging. Traditional Navier-Stokes solvers usually construct multi-resolution body-fitted meshes to achieve high accuracy, often together with near-wall and sub-grid turbulence modeling. However, this could be time-consuming and computationally intensive even with GPU accelerations. An alternative and much faster approach is to switch to a kinetic solver, such as the lattice Boltzmann model, but boundary treatment has to be done in a cut-cell manner, sacrificing accuracy unless grid resolution is much increased. In this paper, we focus on simulating the boundary-dominated turbulent flow phenomena with an efficient kinetic solver. In order to significantly improve the cut-cell-based boundary treatment for higher accuracy without excessively increasing the simulation resolution, we propose a novel parametric boundary treatment model, including a semi-Lagrangian scheme at the wall for non-equilibrium distribution functions, together with a purely link-based near-wall analytical mesoscopic model by analogy with the macroscopic wall modeling approach, which is yet simple to compute. Such a new method is further extended to handle moving boundaries, showing increased accuracy. Comprehensive analyses are conducted, with a variety of simulation results that are both qualitatively and quantitatively validated with experiments and real life scenarios, and compared to existing methods, to indicate superiority of our method. We highlight that our method not only provides a more accurate way for boundary treatment, but also a valuable tool to control boundary layer behaviors. This has not been achieved and demonstrated before in computer graphics, which we believe will be very useful in practical engineering.
用于模拟边界主导湍流现象的参数动力学求解器
边界层流动对流体内部障碍物前后的整体流动特征的形成起着非常重要的作用。因此,边界处理方法对于物理上一致的流体模拟至关重要,特别是当湍流发生在高雷诺数时,在这种情况下,精确处理薄边界层变得非常具有挑战性。传统的Navier-Stokes求解方法通常构建多分辨率体拟合网格,以达到较高的精度,通常与近壁和亚网格湍流建模相结合。然而,即使使用GPU加速,这也可能是耗时和计算密集型的。另一种更快的方法是切换到动力学求解器,如晶格玻尔兹曼模型,但边界处理必须以切割细胞的方式进行,除非网格分辨率大大提高,否则会牺牲精度。在本文中,我们着重于用一个有效的动力学求解器来模拟边界主导的湍流现象。为了在不过度增加模拟分辨率的情况下显著提高基于切胞的边界处理的精度,我们提出了一种新的参数化边界处理模型,包括非平衡分布函数的壁面半拉格朗日格式,以及类比宏观壁面建模方法的纯基于链接的近壁面解析介观模型,该模型计算简单。将这种新方法进一步扩展到处理移动边界,显示出更高的精度。通过对各种仿真结果进行综合分析,并结合实验和实际场景对仿真结果进行定性和定量验证,并与现有方法进行对比,表明了本文方法的优越性。我们强调,我们的方法不仅提供了更精确的边界处理方法,而且是控制边界层行为的有价值的工具。这在计算机图形学中还没有被实现和证明,我们相信这将在实际工程中非常有用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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