We present an accurate and efficient solver for atmospheric dynamics simulations that allows for non-conforming mesh refinement. The model equations are the conservative Euler equations for compressible flows. The numerical method is based on an $h-$adaptive Discontinuous Galerkin spatial discretization and on a second order Additive Runge Kutta IMEX method for time discretization, especially designed for low Mach regimes. The solver is implemented in the framework of the $deal.II$ library, whose mesh refinement capabilities are employed to enhance efficiency. A number of numerical experiments based on classical benchmarks for atmosphere dynamics demonstrate the properties and advantages of the proposed method.
翻译:我们为大气动态模拟提供了一个准确而高效的解决方案,允许不兼容的网状改进。模型方程式是压缩流的保守的 Euler 方程式。数字方法基于美元-美元适应性不连续的Galerkin空间离散和时间分解的第二顺序Aditive Runge Kutta IMEX方法,特别为低马赫制度设计。解决方案是在$deal.II 图书馆的框架内实施的,该图书馆的网状精炼能力被用于提高效率。根据大气动态传统基准进行的若干数字实验显示了拟议方法的特性和优点。