Suppr超能文献

基底加热液滴中乙醇蒸发不稳定性单边数值模型的边界条件。

Boundary conditions for a one-sided numerical model of evaporative instabilities in sessile drops of ethanol on heated substrates.

机构信息

Aix-Marseille University, IUSTI UMR 7343 CNRS, 13453 Marseille, France.

Aix-Marseille University, MADIREL UMR 7246 CNRS, 13013 Marseille, France.

出版信息

Phys Rev E. 2017 Dec;96(6-1):063113. doi: 10.1103/PhysRevE.96.063113. Epub 2017 Dec 19.

Abstract

The work is focused on obtaining boundary conditions for a one-sided numerical model of thermoconvective instabilities in evaporating pinned sessile droplets of ethanol on heated substrates. In the one-sided model, appropriate boundary conditions for heat and mass transfer equations are required at the droplet surface. Such boundary conditions are obtained in the present work based on a derived semiempirical theoretical formula for the total droplet's evaporation rate, and on a two-parametric nonisothermal approximation of the local evaporation flux. The main purpose of these boundary conditions is to be applied in future three-dimensional (3D) one-sided numerical models in order to save a lot of computational time and resources by solving equations only in the droplet domain. Two parameters, needed for the nonisothermal approximation of the local evaporation flux, are obtained by fitting computational results of a 2D two-sided numerical model. Such model is validated here against parabolic flight experiments and the theoretical value of the total evaporation rate. This study combines theoretical, experimental, and computational approaches in convective evaporation of sessile droplets. The influence of the gravity level on evaporation rate and contributions of different mechanisms of vapor transport (diffusion, Stefan flow, natural convection) are shown. The qualitative difference (in terms of developing thermoconvective instabilities) between steady-state and unsteady numerical approaches is demonstrated.

摘要

这项工作专注于为在加热基底上蒸发的固定液滴乙醇的热对流不稳定性的单侧数值模型获得边界条件。在单侧模型中,需要在液滴表面为热传递方程和质量传递方程提供适当的边界条件。在目前的工作中,基于总液滴蒸发率的导出半经验理论公式以及局部蒸发通量的双参数非等温近似,获得了这种边界条件。这些边界条件的主要目的是应用于未来的三维(3D)单侧数值模型中,以便通过仅在液滴域中求解方程来节省大量计算时间和资源。局部蒸发通量的非等温近似所需的两个参数通过拟合二维双侧数值模型的计算结果获得。在此,针对抛物线飞行实验和总蒸发率的理论值对该模型进行了验证。本研究将固定液滴的对流蒸发中的理论、实验和计算方法相结合。展示了重力水平对蒸发率的影响以及不同蒸汽传输机制(扩散、 Stefan 流、自然对流)的贡献。还演示了稳态和非稳态数值方法之间的定性差异(就发展的热对流不稳定性而言)。

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验