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A unified hyperbolic interface capturing scheme for gas-liquid flows

机译:统一的双曲线界面捕获方案

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We present a novel numerical framework for computing multiphase systems with a dense dispersed phase. ^The formulation described solves for a unified, consistent set of conservation equations for the entire flow domain. ^The interface between phases is captured as part of the solution permitting solution of the complex 3D transient evolution of the interface. ^An upwind flux-differenced procedure is developed for generalized thermodynamic state equations which reproduces the correct physical acoustic speed. ^This upwind numerical formulation is also extended to simulate a dense dispersed phase which is in nonequilibrium with the continuum. ^The wave propagation process for these nonequilibrium flows is shown to be physically consistent, and the numerical instability associated with multiphase flows is interpreted as arising from source terms involving gradients of porosity. ^A range of studies, from fundamental shock tubes studies to 3D transient problems are presented. ^In particular, considerable success has been achieved in modeling various combustion instability phenomena in interior ballistic problems where acoustic waves have coupled with liquid propellant combustion to generate high frequency waves. ^(Author)
机译:我们提出了一种新颖的数值框架,用于计算具有密集分散相的多相系统。 ^所描述的公式为整个流域求解了一套统一,一致的守恒方程组。 ^捕获相之间的界面作为解决方案的一部分,从而可以解决界面的复杂3D瞬态演化问题。 ^针对广义热力学状态方程式开发了迎风通量微分程序,该程序可再现正确的物理声速。 ^此逆风数值公式也得到扩展,以模拟与连续体不平衡的稠密分散相。 ^这些非平衡流的波传播过程在物理上是一致的,与多相流有关的数值不稳定性被解释为源于孔隙度梯度的源项。 ^提出了一系列研究,从基础激波管研究到3D瞬态问题。特别是,在对内部弹道问题的各种燃烧不稳定性现象进行建模方面,已经取得了相当大的成功,在这些问题中,声波与液体推进剂燃烧耦合产生高频波。 ^(作者)

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