In Situ Estimation of the Coefficient of Stress Source in the Eulerian–Lagrangian Spray Atomization Model

C. R. L. Anumolu, Ambarish Dahale
{"title":"In Situ Estimation of the Coefficient of Stress Source in the\n Eulerian–Lagrangian Spray Atomization Model","authors":"C. R. L. Anumolu, Ambarish Dahale","doi":"10.4271/2024-01-5069","DOIUrl":null,"url":null,"abstract":"Liquid jet atomization is one of the key processes in many engineering\n applications, such as IC engines, gas turbines, and the like, to name a few.\n Simulating this process using a pure Eulerian or a pure Lagrangian framework has\n its own drawbacks. The Eulerian–Lagrangian spray atomization (ELSA) modeling\n seems like a viable alternative in such scenarios. ELSA simulations consist of\n solving an additional transport equation for the surface area density (Σ) of the\n issuing jet. In this study we have proposed a dynamic approach to compute the\n turbulent timescale constant (α1), which appears in\n the source of Σ-transport equation and is responsible for restoring the surface\n area back to its equilibrium. The dynamic approach involves an analytical\n computation of the turbulent timescale constant\n (α1), thereby eliminating the need for ad hoc\n adjustments to surface area values during computational fluid dynamics (CFD)\n simulations. Unlike previous research which suggests using constant values in\n the range (0, 1] for the α1-constant, we found that\n these values can be as high as 60,000 for the engine combustion network (ECN)\n spray-A nozzle conditions. The analytical closure procedure dampens the spurious\n overshoots seen in the sigma-Y field and maintains values close to the\n equilibrium conditions. The proposed approach is implemented in CONVERGE, a\n commercially available CFD code and validated by comparing against available\n experimental data.","PeriodicalId":510086,"journal":{"name":"SAE Technical Paper Series","volume":"161 4","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-07-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"SAE Technical Paper Series","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4271/2024-01-5069","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Liquid jet atomization is one of the key processes in many engineering applications, such as IC engines, gas turbines, and the like, to name a few. Simulating this process using a pure Eulerian or a pure Lagrangian framework has its own drawbacks. The Eulerian–Lagrangian spray atomization (ELSA) modeling seems like a viable alternative in such scenarios. ELSA simulations consist of solving an additional transport equation for the surface area density (Σ) of the issuing jet. In this study we have proposed a dynamic approach to compute the turbulent timescale constant (α1), which appears in the source of Σ-transport equation and is responsible for restoring the surface area back to its equilibrium. The dynamic approach involves an analytical computation of the turbulent timescale constant (α1), thereby eliminating the need for ad hoc adjustments to surface area values during computational fluid dynamics (CFD) simulations. Unlike previous research which suggests using constant values in the range (0, 1] for the α1-constant, we found that these values can be as high as 60,000 for the engine combustion network (ECN) spray-A nozzle conditions. The analytical closure procedure dampens the spurious overshoots seen in the sigma-Y field and maintains values close to the equilibrium conditions. The proposed approach is implemented in CONVERGE, a commercially available CFD code and validated by comparing against available experimental data.
欧拉-拉格朗日喷雾雾化模型中应力源系数的现场估算
液体喷射雾化是集成电路发动机、燃气轮机等许多工程应用中的关键过程之一。使用纯欧拉或纯拉格朗日框架模拟这一过程有其自身的缺点。在这种情况下,欧拉-拉格朗日喷雾雾化(ELSA)建模似乎是一个可行的替代方案。欧拉-拉格朗日喷雾雾化(ELSA)模拟包括求解一个额外的喷射流表面积密度(Σ)传输方程。在这项研究中,我们提出了一种动态方法来计算湍流时标常数(α1),它出现在 Σ 传输方程的源中,负责将表面积恢复到平衡状态。动态方法涉及湍流时标常数(α1)的分析计算,因此无需在计算流体动力学(CFD)模拟过程中对表面积值进行特别调整。以往的研究建议使用范围在(0,1)内的α1常数,而我们发现,在发动机燃烧网络(ECN)喷雾-A喷嘴条件下,α1常数可高达60,000。分析封闭程序抑制了 sigma-Y 场中出现的虚假过冲,并保持了接近平衡条件的值。建议的方法在 CONVERGE(一种商用 CFD 代码)中实施,并通过与现有实验数据的比较进行了验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信