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Towards front-tracking based on conservation in two space dimensions III, tracking interfaces

机译:走向基于二维空间守恒的前跟踪,跟踪接口

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This is the third paper in the series of our conservative front-tracking method. In this paper, we describe how our method tracks fluid interfaces in multi-fluid flows. Two important ingredients in our conservative front-tracking method in tracking fluid interfaces are: (1) the velocities and pressures of the left and right cell-averages in a discontinuity cell are respectively maintained to be equal to each other, and in doing so the physics that the normal velocity and pressure are continuous cross the interface is simulated but that the tangential velocity may be discontinuous is ignored, and (2) a so-called numerical surface dissipation is designed on the tracked interface to eliminate possible numerical instability there, and we believe that this numerical surface dissipation is a good substitute for the missing physical dissipation acting on the interface. We then present numerical simulation of Haas-Sturtevant's two shock-bubble interaction experiments [J.F. Haas, B. Sturtevant, Interaction of weak shock waves with cylindrical and spherical gas inhomogeneities, J. Fluid Mech. 181 (1987) 41-76] using this method. Our numerical results are in good agreement with the experimental and other numerical results in the early times of the flow. Moreover, our numerical results are also in good agreement with the experimental results in the later times of the flow and give clear pictures of the bubble deformation then, which show that the right boundaries of the bubble behave just as Rychtmyer-Meshkov instabilities with the shock coming from either heavy or light gases.
机译:这是我们保守的前跟踪方法系列的第三篇文章。在本文中,我们描述了我们的方法如何跟踪多流体流中的流体界面。在跟踪流体界面方面,我们保守的前向跟踪方法的两个重要组成部分是:(1)分别将不连续单元中的左,右单元平均速度和压力保持彼此相等,并且在这种情况下,模拟了界面上法向速度和压力是连续的但切向速度可能不连续的物理学原理,并且(2)在被跟踪的界面上设计了所谓的数值表面耗散,以消除在那里可能存在的数值不稳定性,以及我们相信,这种表面数值耗散可以很好地替代作用在界面上的物理耗散。然后,我们介绍了Haas-Sturtevant的两个冲击气泡相互作用实验的数值模拟[J.F. Haas,B. Sturtevant,弱冲击波与圆柱和球形气体不均匀性的相互作用,J。流体力学。 181(1987)41-76]。我们的数值结果与流动早期的实验和其他数值结果非常吻合。此外,我们的数值结果也与流动后期的实验结果非常吻合,并给出了气泡变形的清晰图片,表明气泡的右边界表现为与激波的Rychtmyer-Meshkov不稳定性相同。来自重气体或轻气体。

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