Nelson Nicholas J, Grinstein Fernando F
Los Alamos National Laboratory, Los Alamos, New Mexico 87545, USA.
Phys Rev E Stat Nonlin Soft Matter Phys. 2015 Jul;92(1):013014. doi: 10.1103/PhysRevE.92.013014. Epub 2015 Jul 15.
The mixing of materials due to the Richtmyer-Meshkov instability and the ensuing turbulent behavior is of intense interest in a variety of physical systems including inertial confinement fusion, combustion, and the final stages of stellar evolution. Extensive numerical and laboratory studies of shock-driven mixing have demonstrated the rich behavior associated with the onset of turbulence due to the shocks. Here we report on progress in understanding shock-driven mixing at interfaces between fluids of differing densities through three-dimensional (3D) numerical simulations using the rage code in the implicit large eddy simulation context. We consider a shock-tube configuration with a band of high density gas (SF(6)) embedded in low density gas (air). Shocks with a Mach number of 1.26 are passed through SF(6) bands, resulting in transition to turbulence driven by the Richtmyer-Meshkov instability. The system is followed as a rarefaction wave and a reflected secondary shock from the back wall pass through the SF(6) band. We apply a variety of initial perturbations to the interfaces between the two fluids in which the physical standard deviation, wave number range, and the spectral slope of the perturbations are held constant, but the number of modes initially present is varied. By thus decreasing the density of initial spectral modes of the interface, we find that we can achieve as much as 25% less total mixing at late times. This has potential direct implications for the treatment of initial conditions applied to material interfaces in both 3D and reduced dimensionality simulation models.
由于里希特迈尔-梅什科夫不稳定性导致的材料混合以及随之而来的湍流行为,在包括惯性约束聚变、燃烧和恒星演化最后阶段在内的各种物理系统中引起了极大的关注。对激波驱动混合的广泛数值和实验室研究表明,激波会引发与湍流起始相关的丰富行为。在此,我们报告在隐式大涡模拟背景下使用rage代码通过三维(3D)数值模拟来理解不同密度流体界面处激波驱动混合方面所取得的进展。我们考虑一种激波管配置,其中高密度气体(SF₆)带嵌入在低密度气体(空气)中。马赫数为1.26的激波穿过SF₆带,导致由里希特迈尔-梅什科夫不稳定性驱动的湍流转变。随着稀疏波和来自后壁的反射二次激波穿过SF₆带,对该系统进行跟踪。我们对两种流体之间的界面施加各种初始扰动,其中扰动的物理标准差、波数范围和谱斜率保持不变,但初始存在的模式数量会有所不同。通过这样降低界面初始谱模式的密度,我们发现后期的总混合量可减少多达25%。这对于三维和降维模拟模型中应用于材料界面的初始条件处理具有潜在的直接影响。