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A Mach-number-gradient-based shock switch for accurate computation of inviscid compressible flows

机译:基于MACH-NUMBER-梯度的冲击开关,用于精确计算INCISCID可压缩流动

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In the computation of unsteady Euler equations of gas dynamics the development of numerical schemes that can accurately capture a shock irrespective of its strength or grid-inclination has received considerable research-interest in recent times. Towards this goal multidimensional-upwind schemes have gained popularity. However, these schemes are computationally expensive. The class of self-adjusting-hybrid methods is a promising alternative that can produce multidimensional-like effects with a lower computational cost. Choices of the two schemes for hybridization and the shock switch are two crucial issues that affect the performance of a self-adjusting-hybrid scheme. The design of a robust and versatile shock switch is a crucial issue that affects the performance of a hybrid scheme. Shock switches of varied applicability and complexity have been reported in literature. However, most of the existing shock switches suffer from limitations like requirement of a large stencil-size, dependence on too many user-adjustable parameters and susceptibility to activation near smooth extrema. This paper presents the superior performance of a recently-developed shock switch to obtain a simple, yet robust hybrid method that combines the AUSM and DRLLF schemes. The switch works based on the gradient of contravariant Mach number across neighbouring cell-interfaces. The performance-comparison of the Mach-number-gradient-based switch is done with a popular switch proposed by Swanson and Turkel - taken as the representative of switches that are not based on gradients - using a set of one- and two-dimensional inviscid compressible-flow problems. It is demonstrated that the hybrid scheme produces multidimensional-like effects with the gradient-based switch for the wide range of problems. Further, the performance of Swanson and Turkel's switch is improved by tuning a user-adjustable parameter that depends on the local grid-scale. In that context, the superior qualities of the Mach-number-gradient-based switch are established in terms of its versatility, robustness, a small stencil-size and freedom from user-intervention.
机译:在计算天然气动力学的不稳定欧拉方程的计算中,可以准确地捕获休克的数值方案的发展,而不管其强度或电网倾斜都接受了最近的研究兴趣。迈向这一目标,多百合 - Upwind方案越来越受欢迎。但是,这些方案是计算昂贵的。自调整混合方法的类是一个有前途的替代方案,可以以较低的计算成本产生多维效果。杂交和冲击开关的两种方案的选择是影响自调节混合方案的性能的两个关键问题。坚固且多功能的冲击开关的设计是影响混合动力车方案性能的重要问题。在文献中报告了各种适用性和复杂性的冲击开关。然而,大多数现有的冲击开关患有大型模板大小的要求等限制,依赖于太多的用户可调参数和对光滑的激活易感性。本文介绍了最近开发的冲击开关的卓越性能,以获得结合AUSM和DRLLF方案的简单且坚固的混合方法。交换机基于相邻单元接口跨越逆线Mach数的梯度。基于Mach-Number-梯度的交换机的性能比较是用Swanson和Turkel提出的流行开关完成的 - 使用一组单维和二维INCISCID作为不基于梯度的交换机的代表进行压缩流动问题。据证明,混合动力车方案用基于梯度的开关产生多维效果,用于广泛的问题。此外,通过调整取决于本地网格级的用户可调参数,改善了Swanson和Turkel交换机的性能。在这种情况下,基于Mach-Number梯度的交换机的卓越品质是根据其多功能性,鲁棒性,小模板尺寸和来自用户干预的自由度来建立的。

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