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A parallel unstructured dynamic mesh adaptation algorithm for 3-D unsteady flows

机译:3-D非定常流的并行非结构化动态网格自适应算法

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摘要

An unstructured dynamic mesh adaptation and load balancing algorithm has been developed for the efficient simulation of three-dimensional unsteady inviscid flows on parallel machines. The numerical scheme was based on a cell-centred finite-volume method and the Roe's flux-difference splitting. Second-order accuracy was achieved in time by using an implicit Jacobi/Gauss-Seidel iteration. The resolution of time-dependent solutions was enhanced by adopting an h-refinement/coarsening algorithm. Parallelization and load balancing were concurrently achieved on the adaptive dynamic meshes for computational speed-up and efficient memory redistribution. A new tree data structure for boundary faces was developed for the continuous transfer of the communication data across the parallel subdomain boundary. The parallel efficiency was validated by applying the present method to an unsteady shock-tube problem. The flows around oscillating NACA0012 wing and F-5 wing were also calculated for the numerical verification of the present dynamic mesh adaptation and load balancing algorithm. Copyright © 2005 John Wiley & Sons, Ltd.
机译:已经开发了一种非结构化动态网格自适应和负载平衡算法,用于在并行计算机上高效地模拟三维非定常无粘性流。数值方案基于单元中心有限体积方法和Roe的磁通量差分裂。通过使用隐式Jacobi / Gauss-Seidel迭代可以及时达到二阶精度。通过采用h细化/粗化算法,可以提高与时间有关的解决方案的分辨率。在自适应动态网格上同时实现了并行化和负载平衡,以提高计算速度和有效地重新分配内存。开发了一种用于边界面的新树数据结构,用于跨并行子域边界连续传输通信数据。通过将本方法应用于不稳定的激波管问题,可以验证并行效率。还计算了围绕NACA0012机翼和F-5机翼摆动的气流,以对当前的动态网格自适应和负载平衡算法进行数值验证。版权与复制; 2005年John Wiley&Sons,Ltd.

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