LES Prediction of the Ignition Probability Map for a Model Aeronautical Spray Burner

IF 2.4 3区 工程技术 Q3 MECHANICS Flow, Turbulence and Combustion Pub Date : 2024-12-11 DOI:10.1007/s10494-024-00617-4
Ernesto Sandoval Garzon, Cédric Mehl, Olivier Colin
{"title":"LES Prediction of the Ignition Probability Map for a Model Aeronautical Spray Burner","authors":"Ernesto Sandoval Garzon,&nbsp;Cédric Mehl,&nbsp;Olivier Colin","doi":"10.1007/s10494-024-00617-4","DOIUrl":null,"url":null,"abstract":"<div><p>This study presents the computation of the ignition probability map of a model gas turbine, investigated experimentally at CORIA laboratory, using Large Eddy Simulation (LES). The simulations leverage the recently proposed TFM-AMR-I model, which is based on the Thickened Flame Model (TFM) formalism and enables a full flame resolution (i.e. no thickening) of the flame kernel in the initial instants of ignition. LES simulations of ignition are performed for 14 spatial points distributed in the combustion chamber, with 6 repetitions for each in order to obtain a reasonable estimate of ignition probabilities. Probabilities are adequately predicted for most of the selected points, with a typical error of 30 <span>\\(\\%\\)</span>. Nevertheless, the ignition probability is largely over-estimated at two locations where the mean diameter of liquid droplets is shown to be under-predicted, which may lead to too easy ignitions. Parametric variations show a satisfying robustness of the proposed approach with the two following key highlights: (i) the initial full flame resolution made possible by TFM-AMR-I is necessary, as an abrupt initial thickening leads to an artificial extinction; (ii) a correction of the over-sensitivity of the thickened flame to stretch, recently proposed in the literature, is necessary to predict ignition accurately.</p></div>","PeriodicalId":559,"journal":{"name":"Flow, Turbulence and Combustion","volume":"114 2","pages":"449 - 467"},"PeriodicalIF":2.4000,"publicationDate":"2024-12-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Flow, Turbulence and Combustion","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s10494-024-00617-4","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0

Abstract

This study presents the computation of the ignition probability map of a model gas turbine, investigated experimentally at CORIA laboratory, using Large Eddy Simulation (LES). The simulations leverage the recently proposed TFM-AMR-I model, which is based on the Thickened Flame Model (TFM) formalism and enables a full flame resolution (i.e. no thickening) of the flame kernel in the initial instants of ignition. LES simulations of ignition are performed for 14 spatial points distributed in the combustion chamber, with 6 repetitions for each in order to obtain a reasonable estimate of ignition probabilities. Probabilities are adequately predicted for most of the selected points, with a typical error of 30 \(\%\). Nevertheless, the ignition probability is largely over-estimated at two locations where the mean diameter of liquid droplets is shown to be under-predicted, which may lead to too easy ignitions. Parametric variations show a satisfying robustness of the proposed approach with the two following key highlights: (i) the initial full flame resolution made possible by TFM-AMR-I is necessary, as an abrupt initial thickening leads to an artificial extinction; (ii) a correction of the over-sensitivity of the thickened flame to stretch, recently proposed in the literature, is necessary to predict ignition accurately.

Abstract Image

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
航空喷射器模型点火概率图的LES预测
本文采用大涡模拟(Large Eddy Simulation, LES)方法对某型号燃气轮机点火概率图进行了计算。模拟利用了最近提出的TFM- amr - i模型,该模型基于增厚火焰模型(TFM)的形式,并在点火的初始时刻实现火焰核的完全火焰分辨率(即没有增厚)。为了得到合理的点火概率估计,对分布在燃烧室内的14个空间点进行了LES点火模拟,每个点重复6次。对大多数选定点的概率进行了充分的预测,典型误差为30 \(\%\)。然而,在液滴平均直径被低估的两个位置,点火概率在很大程度上被高估了,这可能导致太容易点火。参数变化表明该方法具有令人满意的鲁棒性,具有以下两个关键亮点:(i) TFM-AMR-I实现的初始全火焰分辨率是必要的,因为突然的初始增厚会导致人工消光;(ii)最近在文献中提出的对加厚火焰对拉伸的过度敏感性的修正是准确预测点火的必要条件。
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 去求助
来源期刊
Flow, Turbulence and Combustion
Flow, Turbulence and Combustion 工程技术-力学
CiteScore
5.70
自引率
8.30%
发文量
72
审稿时长
2 months
期刊介绍: Flow, Turbulence and Combustion provides a global forum for the publication of original and innovative research results that contribute to the solution of fundamental and applied problems encountered in single-phase, multi-phase and reacting flows, in both idealized and real systems. The scope of coverage encompasses topics in fluid dynamics, scalar transport, multi-physics interactions and flow control. From time to time the journal publishes Special or Theme Issues featuring invited articles. Contributions may report research that falls within the broad spectrum of analytical, computational and experimental methods. This includes research conducted in academia, industry and a variety of environmental and geophysical sectors. Turbulence, transition and associated phenomena are expected to play a significant role in the majority of studies reported, although non-turbulent flows, typical of those in micro-devices, would be regarded as falling within the scope covered. The emphasis is on originality, timeliness, quality and thematic fit, as exemplified by the title of the journal and the qualifications described above. Relevance to real-world problems and industrial applications are regarded as strengths.
期刊最新文献
Publisher Correction to: Direct, large eddy, and Reynolds-averaged Navier-Stokes simulations of hydrogen periodic planar jets in argon Prediction of Laminar Separation Bubble on Airfoils at Low Reynolds Number Assessment of the PODFS Inlet Turbulence Generation Approach in LES of Bluff-Body Flow and Heat Transfer Numerical Study on Operation Modes, Operational Characteristics, and Propulsion Performance of Rotating Detonation Engines Cyclic Spark-Ignition Versus Self-Ignition Phenomena in Constant Volume Combustors
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1