Numerical investigation on characteristics of interfacial wave of liquid film in gas–liquid two-phase flow using OpenFOAM

IF 6.9 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Chinese Journal of Aeronautics Pub Date : 2024-02-01 Epub Date: 2023-08-20 DOI:10.1016/j.cja.2023.08.010
Xiaoqi MA, Yueshe WANG, Jiaming TIAN
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引用次数: 0

Abstract

Liquid film cooling as an advanced cooling technology is widely used in space vehicles. Stable operation of liquid film along the rocket combustion inner wall is crucial for thermal protection of rocket engines. The stability of liquid film is mainly determined by the characteristics of interfacial wave, which is rarely investigated right now. How to improve the stability of thin film has become a hot spot. In view of this, an advanced model based on the conventional Volume of Fluid (VOF) model is adopted to investigate the characteristics of interfacial wave in gas–liquid flow by using OpenFOAM, and the mechanism of formation and development of wave is revealed intuitively through numerical study. The effects from gas velocity, surface tension and dynamic viscosity of liquid (three factors) on the wave are studied respectively. It can be found that the gas velocity is critical to the formation and development of wave, and four modes of droplets generation are illustrated in this paper. Besides, a gas vortex near the gas–liquid interface can induce formation of wave easily, so changing the gas vortex state can regulate formation and development of wave. What’s more, the change rules of three factors influencing on the interfacial wave are obtained, and the surface tension has a negative effect on the formation and development of wave only when the surface tension coefficient is above the critical value, whereas the dynamic viscosity has a positive effect in this process. Lastly, the maximum height and maximum slope angle of wave will level off as the gas velocity increases. Meanwhile, the maximum slope angle of wave is usually no more than 38°, no matter what happens to the three factors.

基于OpenFOAM的气液两相流液膜界面波特性数值研究
液膜冷却作为一种先进的冷却技术被广泛应用于航天器中。火箭燃烧内壁液膜的稳定运行对火箭发动机的热保护至关重要。液膜的稳定性主要取决于界面波的特性,而目前对界面波特性的研究还很少。如何提高薄膜的稳定性已成为研究热点。有鉴于此,本文在传统流体体积(VOF)模型的基础上,利用 OpenFOAM 建立了一个先进的模型来研究气液流动中界面波的特性,并通过数值研究直观地揭示了波的形成和发展机理。分别研究了气体速度、表面张力和液体动态粘度(三个因素)对波的影响。结果表明,气体速度对波浪的形成和发展至关重要,本文阐述了四种液滴生成模式。此外,气液界面附近的气体漩涡很容易诱发波的形成,因此改变气体漩涡状态可以调节波的形成和发展。此外,本文还得出了影响界面波的三个因素的变化规律,只有当表面张力系数大于临界值时,表面张力才会对界面波的形成和发展产生负面影响,而动态粘度则会在此过程中产生正面影响。最后,随着气体速度的增加,波浪的最大高度和最大斜角会趋于平缓。同时,无论这三个因素如何变化,波浪的最大斜角通常不超过 38°。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
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