论文标题
通过湍流流动液膜的空气动力学驱动的破裂
Aerodynamically-driven rupture of a liquid film by turbulent shear flow
论文作者
论文摘要
使用流体量方法研究了由于气相中共同流动的湍流剪切流而导致的液体膜破裂。为了模拟这种多相问题,我们使用简化的数值设置,其中液膜是从湍流通道模拟的两个完全开发的边界层之间“夹在”的。这部电影变形并最终在由共同流程产生的剪切区域内破裂。这种有效的设置允许物理参数的系统变化,以衡量其在完全发育的剪切湍流下液体膜的空气动力驱动变形和破裂的作用。本工作介绍了对变形膜和相关空气动力效应的发展压力场的详细研究,如其他作者先前所建议的,特别是Inviscid Lift和阻力力的作用。引入了累积的升力力,以捕获膜上交替压力最小值和最大值形成的效果,从而放大并最终破裂膜。从升力引起的拖曳力得出的速度量表反映了膜上湍流边界层的状态,并崩溃了这种累积的升力力的时间发育以及膜变形的幅度,对于不同的膜厚度和雷诺数的成功,并获得了一些成功。
The rupture of a liquid film due to co-flowing turbulent shear flows in the gas phase is studied using a volume-of-fluid method. To simulate this multiphase problem, we use a simplified numerical setup where the liquid film is 'sandwiched' between two fully developed boundary layers from a turbulent channel simulation. The film deforms and eventually ruptures within the shear zone created by the co-flows. This efficient setup allows systematic variation of physical parameters to gauge their role in the aerodynamically-driven deformation and rupture of a liquid film under fully developed sheared turbulence. The present work presents a detailed study of the developing pressure field over the deforming film and related aerodynamic effects, as previously suggested by other authors, in particular the role of the inviscid lift and drag forces. A cumulative lift force is introduced to capture the effect of the alternating pressure minima and maxima forming over the film which amplify and eventually rupture the film. A velocity scale derived from the lift-induced drag force reflects the state of the turbulent boundary layer over the film and collapses the temporal development of this cumulative lift force as well as the amplitude of film deformation with some success for the different film thicknesses and Reynolds numbers.