Numerical Solution of the 2D Compressible Euler Equations Based on the Unstructured Adaptive Grids
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摘要: 提出了一种基于非结构自适应网格的二维Euler方程的数值解法.采用有限体积法进行空间离散,通量计算采用Jamson中心格式,使得它适用于任意多边形计算单元.为了得到定常解,采用一种显式的四步Runge-Kutta迭代方法对时间进行积分.根据流场参数的变化梯度确定加密边,由加密准则进行自适应网格剖分, 然后得到分布合理的加密过后的网格.求解二维Euler方程,对NACA0012翼型进行了数值模拟,通过对自适应前后的数值解的对比,说明所建立的方法是正确的.Abstract: A numerical method for the solution of the 2D Euler equations based on the unstructured adaptive grids was proposed. The finite-volume method was used to carry out the space discretization, and the flux was calculated with Jamson’s central scheme, which was suitable for the calculation of arbitrary polygons. In order to get the stationary solution, an explicit 4-step Runge-Kutta iterative method was adopted to do the time-domain integral. According to the gradients of the flow field parameters, the refining edges were determined. Under this refining criterion, the mesh distribution was reasonably improved. With the proposed method the 2D Euler equations were solved for the simulation of the NACA0012 airfoil. The numerical results show the correctness and validity of the present method.
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Key words:
- Euler equation /
- numerical solution /
- unstructured grid /
- adaptive mesh refinement
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