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

机译:组合涡旋内和并行快速多极方法以实现有效的域分解模拟

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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) flow; 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-unbounded) 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:提出了一种新的涡旋内和并联快速多极方法的组合,其允许有效地模拟并行,无界和半无界面的涡流(用一个平坦的墙壁流动)。在经典的涡流(VIC)方法中,用于解决泊松方程的网格通常比涡旋场区域大得多,以便能够强加适当的远场边界条件,从而近似真实的远场边界条件,从而逼近无限的(或半无界)流动;另一种方法是假设周期性。这种方法导致解决方案,这取决于全局网格尺寸,对于巨大的问题,对无法管理的内存和CPU要求。这里利用的想法是在一个域上工作,该域紧紧包含涡旋字段,并且可以在使用并行快速多极(PFM)方法获得精确边界条件的若干子域中进行分解。这通常求解3-D泊松方程,而不需要子域之间的任何迭代(例如,无需施瓦茨迭代):这是因为PFM方法具有整个涡卷场的全局视图,满足远场条件。通过该VIC-PFM组合获得的溶液然后对应于真正无界(或半未束缚)流的模拟。与单独使用(2)单独使用PFM求解器的涡流粒子方法,与使用(2)单独使用PFM求解器的涡流颗粒方法,需要更少的存储器,并导致更好的计算效率。提出了3-D无界的流量验证结果:不稳定性,非线性演化和涡旋环的衰减(首先使用该方法的顺序版本的中等雷诺数,然后使用并行版本处的高雷诺数);两个涡旋系统在地面效果中的不稳定和非线性演变。最后,还提出了在地面效果中的飞机涡旋唤醒的空间开发模拟。 (c))2007年elestvier Inc.保留所有权利。

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