{"title":"HEAT AND MASS TRANSFER CONTROL BY EVAPORATIVE THERMAL PATTERNING OF THIN LIQUID LAYERS","authors":"C. Iorio, O. Goncharova, O. Kabov","doi":"10.1615/COMPUTTHERMALSCIEN.2011003229","DOIUrl":null,"url":null,"abstract":"For several years, interfacial instabilities arising in evaporating layers of volatile liquid when subjected to a shear flow of inert and non-absorptive gas have been studied for their intrinsic complexity due to the interaction between different phenomena such as heat and mass transfer through the layer interface, thermo-capillarity, natural convection, and shear-induced stresses. More recently, the possibility of generating ordered thermal patterns in an evaporating layer by controlling such kinds of instabilities has been considered as an intriguing technique to enhance heat and mass transfer in precisely defined spots at the interface of the layers. We studied numerically the topology of the thermal patterns as well as the heat and mass transfer characteristics that can be induced in an evaporating liquid layer by controlling the thickness of the layer while keeping constant the gas flow intensity. Calculations have been conducted by considering ethanol as the working fluid and nitrogen as the inert gas. The thickness of the layer was varied in order to have aspect ratios with respect to the characteristic length of the evaporating interface in the range of 0.02-1. The inspiring reason for performing the simulations reported in this paper is the preparation of the CIMEX-1 experiment that will be performed on-board the International Space Station in the next future. For that reason, all the calculations presented refer to the condition of the absence of gravity. © 2011 by Begell House, Inc.","PeriodicalId":45052,"journal":{"name":"Computational Thermal Sciences","volume":"3 1","pages":"333-342"},"PeriodicalIF":1.3000,"publicationDate":"2011-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1615/COMPUTTHERMALSCIEN.2011003229","citationCount":"39","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Computational Thermal Sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1615/COMPUTTHERMALSCIEN.2011003229","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"THERMODYNAMICS","Score":null,"Total":0}
引用次数: 39
通过薄液体层的蒸发热模式控制传热传质
多年来,人们一直在研究挥发性液体蒸发层在受到惰性和非吸收性气体剪切流动时产生的界面不稳定性,因为它们的内在复杂性是由于不同现象之间的相互作用,如通过层界面的传热传质、热毛细作用、自然对流和剪切诱导应力。最近,通过控制这种不稳定性在蒸发层中产生有序热模式的可能性被认为是一种有趣的技术,可以在层的界面上精确定义的点上增强传热和传质。本文通过数值模拟研究了在一定气体流动强度的情况下,控制蒸发液层厚度所产生的热模式拓扑结构和传热传质特性。以乙醇为工质,氮气为惰性气体进行了计算。为了使蒸发界面特征长度的纵横比在0.02-1范围内,改变了层的厚度。执行本文中报道的模拟的鼓舞人心的原因是准备CIMEX-1实验,该实验将在未来的国际空间站上进行。因此,所有的计算都是在没有重力的情况下进行的。©2011 by Begell House, Inc。
本文章由计算机程序翻译,如有差异,请以英文原文为准。