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Anisotropic grid refinement using an unstructured discontinuous galerkin method for the three-dimensional euler equations of gas dynamics

机译:使用非结构非连续Galerkin方法对气体动力学三维欧拉方程进行各向异性网格细化

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A numerical method for the solution of the Eulerequations of gas dynamics using anisotropic grid refinement of an unstructured, hexahedron type grid is presented. The discontinuous Galerking finite element method is used to solve the Euler equations in three dimensions. Special attention is paid to the data structure and searching algorithms necessary for efficient calculation on highly irregular grids obtained with local grid refinement. The method is demonstrated with calculations of transonic flow on the ONERA M6 wing.
机译:提出了一种利用非结构化六面体网格的各向异性网格细化方法求解气体动力学欧拉方程的数值方法。不连续的Galerking有限元方法用于求解三维Euler方程。对于通过局部网格细化获得的高度不规则网格的有效计算,必须特别注意必要的数据结构和搜索算法。通过计算ONERA M6机翼上的跨音速流动来演示该方法。

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