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Theoretical model for swirling thin film flows inside nozzles with converging-diverging shapes

机译:薄膜在喷嘴内呈收敛-发散状的涡流理论模型

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A quasi-one-dimensional model was developed to describe a swirling, thin, liquid film inside nozzles with different wall profiles. The model quantifies the effects of swirl strength, initial film thickness, and Reynolds and Weber numbers on the film thickness along the nozzle surface. Moreover, the model allows for a rapid (at least, qualitative) evaluation of different effects, e.g. of the swirl strength and nozzle geometry, and can serve as a benchmark case for the subsequent more involved numerical simulations. Steady-state solutions are presented as a function of various parameters. The effect of the nozzle geometry on film thickness is explored. As swirling flow entered the expanding (diverging) section of the nozzle, film thickness decreased to satisfy continuity (to conserve mass). Conversely, film thickness increased upon entering the contracting (converging) region of the nozzle. Geometric effects controlled film thicknesses much more than other flow parameters. This quasi-one-dimensional model for a swirling thin film can be useful for designing a swirl jet used in various industrial applications. (C) 2019 Elsevier Inc. All rights reserved.
机译:开发了一个准一维模型来描述具有不同壁轮廓的喷嘴内部的旋涡状薄液膜。该模型量化了旋流强度,初始薄膜厚度以及雷诺和韦伯数对沿喷嘴表面的薄膜厚度的影响。而且,该模型允许快速(至少,定性)评估不同的作用,例如。旋流强度和喷嘴几何形状的变化,可以作为后续更复杂的数值模拟的基准案例。稳态解决方案是各种参数的函数。探索了喷嘴几何形状对薄膜厚度的影响。随着旋流进入喷嘴的膨胀(发散)部分,膜厚减小,以满足连续性(节省质量)。相反,膜厚度在进入喷嘴的收缩(会聚)区域时增加。几何效应控制的薄膜厚度远大于其他流动参数。这种用于涡旋薄膜的准一维模型可用于设计各种工业应用中使用的涡旋射流。 (C)2019 Elsevier Inc.保留所有权利。

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