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Combining the vortex-in-cell and parallel fast multipole methods for efficient domain decomposition simulations

机译:结合单元涡旋和并行快速多极方法进行有效的域分解仿真

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A new combination of vortex-in-cell and parallel fast multipole methods is presented which allows to efficiently simulate, in parallel. unbounded and half-unbounded vortical flows (flows with one flat wall). In the classical vortex-in-cell (VIC) method. the grid used to solve the Poisson equation is typically taken Much larger than the vorticity field region, so as to be able to impose suitable far-field boundary conditions and thus approximate the truly unbounded (or half-unbounded) flown an alternative is to assume periodicity. This approach leads to a solution that depends on the global grid size and, for large problems, to unmanageable memory and CPU requirements. The idea exploited here is to work on a domain that contains tightly the vorticity field and that can be decomposed in several subdomains on which the exact boundary conditions are obtained using the parallel fast multipole (PFM) method. This amounts to solving a 3-D Poisson equation without requiring any iteration between the subdomains (e.g., no Schwarz iteration required): this is so because the PFM method has a global view of the entire vorticity field and satisfies the far-field condition. The solution obtained by this VIC-PFM combination then corresponds to the Simulation of a truly unbounded (or half-unnbounded) flow. It requires far less memory and leads to a far better computational efficiency compared to simulations done using either (1) the VIC method alone, or (2) the vortex particle method with PFM solver alone. 3-D unbounded flow validation results are presented: instability, non-linear evolution and decay of a vortex ring (first at a moderate Reynolds number using the sequential version of the method, then at a high Reynolds number using the parallel version); instability and non-linear evolution of a two vortex system in ground effect. Finally, a space-developing simulation of an aircraft vortex wake in ground effect is also presented. (C) 2007 Elsevier Inc. All rights reserved.
机译:提出了单元内涡旋和并行快速多极方法的新组合,该方法允许并行高效地进行仿真。无界和半无界的涡流(具有一个平坦壁的流)。在经典的单元涡旋(VIC)方法中。通常用来求解泊松方程的网格要比涡旋场区域大得多,以便能够施加适当的远场边界条件,从而近似于飞行的真正无界(或半无界)周期性。这种方法导致了一种解决方案,该解决方案取决于全局网格的大小,并且对于较大的问题,取决于难以管理的内存和CPU需求。此处利用的思想是在一个紧密包含涡度场的域中工作,该域可以分解为几个子域,在这些子域中可以使用并行快速多极(PFM)方法获得精确的边界条件。这相当于解决了3-D泊松方程,而无需在子域之间进行任何迭代(例如,不需要Schwarz迭代):之所以如此,是因为PFM方法对整个涡度场具有全局视图并满足远场条件。然后,通过这种VIC-PFM组合获得的解对应于真正无界(或半无界)流的模拟。与仅使用(1)VIC方法或(2)仅使用PFM求解器的涡旋粒子方法进行的仿真相比,它所需的内存少得多,并导致更高的计算效率。提出了3-D无界流动验证结果:涡环的不稳定性,非线性演化和衰减(首先使用该方法的顺序版本以中等的雷诺数,然后使用并行版本以高的雷诺数);地面效应中两个涡旋系统的不稳定性和非线性演化。最后,还提出了飞机涡流在地面效应中的空间发展模拟。 (C)2007 Elsevier Inc.保留所有权利。

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