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超音速高阶面元法软件的可扩并行化

Scalable Parallelization of the Supersonic High-Order Panel Software
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摘要 计算空气动力学的高阶面元法中,将原来位流升力面理论中求解积分方程的问题近似改成求解一组线性代数方程组。针对系数矩阵的特点,采用与所分网络块对应的数据分配方式,并用部分选主元的Gaus-Jordan算法求逆。分别在4台和8台Pentium166微机组成的并行虚拟机(PVM)上运行。当矩阵阶达到2100时,并行效率分别为95.4%和91%。 The high-rder panel method of Computation Fluid Dynamics (CFD) is to approximately turn the problem of solving an integral equation in the potential lift surface theory into solving a linear equation set. We distribute data according to its distributed network blocks because of the characteristic of its coefficient matrix, and use the partially pivoting Gauss-Jordan inversion algorithm. We run it on the Parallel Virtual Machines ( PVM) by 4 or 8 Pentium 166 machine. The result shows that the parallel efficiency is 95.4% and 91% respectively when the matrix order is up to 2100.
出处 《计算机工程与设计》 CSCD 北大核心 1998年第6期58-63,共6页 Computer Engineering and Design
关键词 高阶面元法 求逆算法 PVM 空气动力学 软件 High-order panel method Gauss-Jordan inversion algorithm PVM
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参考文献5

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