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Testing the Hypotheses on Improvement of Iterative Methods Convergence in Solving the Gas Dynamics System of Equations with Optimal Selection of Initial Approximation

机译:以最佳选择初始近似求解方程气体动力学系统的迭代方法收敛性的提高

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The work is devoted to the study of supposed increase in the convergence rate of iterative methods for solving the Navier-Stokes equations depending on selection of the initial approximation. Initial approximation was obtained by numerically integrating the system of gas dynamics equations on a coarse structured curvilinear grid using the finite volume method. Detailed grid consisted of the 10-fold higher number of nodes; and the nodes in the detailed grid generally did not coincide with the nodes in the coarse grid. Results obtained were interpolated onto the detailed grid using the Shepard method (inverse weighted average distance) with a quadratic weight function. Quadratic function in the experiment with known data demonstrated the lowest approximation error. The detailed grid nodes were localized in the cells of a coarse grid using the method of angles summation modified to accelerate the performance. Parameters interpolation in the nodes located on the surface of a body was carried out by pulling nodes of the detailed grid into the wall area of the coarse grid. After interpolating the parameters, calculation was continued on the detailed grid using the same numerical method. Application of the initial approximation from the coarse grid demonstrates an almost 3-fold acceleration of convergence of the numerical solution on a grid condensed by 10 times compared to approximation by the incident flow parameters.
机译:根据选择初始近似的选择,该工作致力于研究求解Navier-Stokes方程的迭代方法的收敛速度的研究。通过使用有限体积法在粗糙的结构化曲线网格上的气体动力学方程数值上与粗糙结构化曲线网格的数量数字集成来获得初始近似。详细的网格由10倍的节点组成;详细网格中的节点通常与粗略网格中的节点不一致。使用二次重量函数(逆加权平均距离)在详细的网格中插入所得结果。具有已知数据的实验中的二次函数展示了最低近似误差。使用变形的角度求和的方法来加速性能,将详细的网格节点定位在粗网格的单元中。位于主体表面上的节点中的参数插值是通过将详细网格的节点拉到粗网格的壁面积中来执行。在内插参数后,使用相同的数字方法在详细网格上继续计算。与粗栅格的初始近似值在与入射流动参数的近似相比,在10次上凝结的网格上的数值溶液的收敛性几乎3倍。

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