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首页> 外文期刊>SIAM Journal on Numerical Analysis >Variational barrier method of adaptive grid generation in hyperbolic problems of gas dynamics
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Variational barrier method of adaptive grid generation in hyperbolic problems of gas dynamics

机译:气体动力学双曲问题中自适应网格生成的变分屏障方法

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摘要

Application of the harmonic mapping using a variational approach to generate moving adaptive grids in the hyperbolic problems of gas dynamics is considered. Using the example of a three-point model of adaptation, the possibility to generate an unfolded mesh with strong grid lines condensing in the vicinity of discontinuities of the control/(monitor) function is demonstrated. The algorithm of redistributing the boundary nodes is suggested and consists of using constrained minimization of the discrete harmonic functional when constraints de ne the boundary of the domain. In real computations due to mesh adaptation it is possible to reduce the errors, caused by shock waves smearing over the cells, by many factors of ten. Modeling of the two-dimensional (2-D) supersonic gas flow in the channel has shown that the same accuracy on the adaptive grid with the same structure as the quasi-uniform mesh can be acheived while requiring less CPU memory by a factor of 25 and less running time by a factor of 50 to 60. Computational tests of the steady transonic and supersonic flow over an airfoil demonstrate the ability of the method to control mesh sizes across shocks. [References: 41]
机译:考虑了在气体动力学的双曲问题中使用变分法的谐波映射在移动自适应网格生成中的应用。以三点自适应模型为例,证明了生成具有强大网格线的未折叠网格的可能性,这些网格线在控制/(监控)功能的不连续性附近凝结。提出了重新分配边界节点的算法,该算法包括在约束定义域边界时使用离散谐波函数的约束最小化。在实际的计算中,由于网格自适应,可以将冲击波拖曳到单元格上所引起的误差降低十分之一。对通道中的二维(2-D)超音速气流的建模表明,在具有与准均匀网格相同的结构的自适应网格上,可以实现相同的精度,而所需的CPU内存则减少了25倍且运行时间减少了50到60倍。对机翼上稳定的跨音速和超音速流的计算测试表明,该方法能够控制整个冲击波的网格大小。 [参考:41]

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