The effect of crossflow perturbations on streaks in laminar boundary layer flames

IF 5.9 2区 工程技术 Q2 ENERGY & FUELS
Combustion and Flame Pub Date : 2026-05-01 Epub Date: 2026-02-19 DOI:10.1016/j.combustflame.2026.114867
Francisco C. Martins, José L.M. Rocha, José C.F. Pereira
{"title":"The effect of crossflow perturbations on streaks in laminar boundary layer flames","authors":"Francisco C. Martins,&nbsp;José L.M. Rocha,&nbsp;José C.F. Pereira","doi":"10.1016/j.combustflame.2026.114867","DOIUrl":null,"url":null,"abstract":"<div><div>This study analyses the dynamics of streaks in laminar boundary layer flames by direct numerical simulation, under three crossflow perturbation states: unperturbed, perturbed by freestream turbulence <span><math><mrow><mo>(</mo><mn>0</mn><mo>.</mo><mn>03</mn><mtext>%</mtext><mo>≤</mo><mi>T</mi><mi>I</mi><mo>≤</mo><mn>1</mn><mtext>%</mtext><mo>)</mo></mrow></math></span>, and perturbed by a steady sinusoidal mimicking manufactured streaks. Simulations reveal that streak behaviour is highly dependent on the perturbation state. Unperturbed crossflows result in delayed streak onset and produce smaller meandering streaks that remain unsteady. Heat flux to the surface below the flame remains uniform in these conditions, due to the small streak amplitude. Freestream turbulence induces earlier onset, increases streak wavenumber, and results in larger flame surface perturbation amplitudes. Streak growth rates are consistent with quadratic scaling typical of Rayleigh–Taylor instability for <span><math><mrow><mi>T</mi><mi>I</mi><mo>≥</mo><mn>0</mn><mo>.</mo><mn>6</mn><mtext>%</mtext></mrow></math></span>, but, for lower <span><math><mrow><mi>T</mi><mi>I</mi></mrow></math></span>, the instability amplitude remains in the regime where growth is governed by Linear Stability Theory scaling. Steady sinusoidal perturbations can be used to control the number of streaks generated, which align with crossflow velocity valleys. For low wavenumber sinusoidal perturbations <span><math><mrow><mo>(</mo><mi>k</mi><mo>&lt;</mo><mn>4</mn><mo>)</mo></mrow></math></span>, larger quasi-steady streaks are overlapped by smaller unsteady meandering streaks. Larger sinusoidal perturbation wavenumbers <span><math><mrow><mo>(</mo><mi>k</mi><mo>≥</mo><mn>4</mn><mo>)</mo></mrow></math></span> induce large steady streaks that separate into finger-like structures, inside which fuel packets are carried downstream and combustion continues. This has a strong influence on estimated heat flux to the bottom surface, which is initially stronger below troughs, due to the lower flame standoff distance, but the contrary is true once the finger-like structures develop.</div><div><strong>Novelty and significance statement</strong></div><div>Boundary layer flames are a largely unexplored setup of reactive flows, especially in the laminar regime. This study features the first simulations of laminar boundary layer flames, addressing the role of crossflow perturbation state on streak development and growth, which is a major gap in the literature left by previous experimental studies. Results confirm the presence of Rayleigh–Taylor instabilities, and show that the perturbation introduced determines perturbation growth and wavenumber, and greatly influences heat flux to nearby surfaces.</div><div>The fundamental physical insights revealed provide key improvements in the understanding of fuel consumption and heating of nearby surfaces. Practical applications that rely on this include wildfire propagation in wind-driven scenarios, and diffusion flame engineering setups.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"287 ","pages":"Article 114867"},"PeriodicalIF":5.9000,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218026001033","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2026/2/19 0:00:00","PubModel":"Epub","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0

Abstract

This study analyses the dynamics of streaks in laminar boundary layer flames by direct numerical simulation, under three crossflow perturbation states: unperturbed, perturbed by freestream turbulence (0.03%≤TI≤1%), and perturbed by a steady sinusoidal mimicking manufactured streaks. Simulations reveal that streak behaviour is highly dependent on the perturbation state. Unperturbed crossflows result in delayed streak onset and produce smaller meandering streaks that remain unsteady. Heat flux to the surface below the flame remains uniform in these conditions, due to the small streak amplitude. Freestream turbulence induces earlier onset, increases streak wavenumber, and results in larger flame surface perturbation amplitudes. Streak growth rates are consistent with quadratic scaling typical of Rayleigh–Taylor instability for TI≥0.6%, but, for lower TI, the instability amplitude remains in the regime where growth is governed by Linear Stability Theory scaling. Steady sinusoidal perturbations can be used to control the number of streaks generated, which align with crossflow velocity valleys. For low wavenumber sinusoidal perturbations (k<4), larger quasi-steady streaks are overlapped by smaller unsteady meandering streaks. Larger sinusoidal perturbation wavenumbers (k≥4) induce large steady streaks that separate into finger-like structures, inside which fuel packets are carried downstream and combustion continues. This has a strong influence on estimated heat flux to the bottom surface, which is initially stronger below troughs, due to the lower flame standoff distance, but the contrary is true once the finger-like structures develop.
Novelty and significance statement
Boundary layer flames are a largely unexplored setup of reactive flows, especially in the laminar regime. This study features the first simulations of laminar boundary layer flames, addressing the role of crossflow perturbation state on streak development and growth, which is a major gap in the literature left by previous experimental studies. Results confirm the presence of Rayleigh–Taylor instabilities, and show that the perturbation introduced determines perturbation growth and wavenumber, and greatly influences heat flux to nearby surfaces.
The fundamental physical insights revealed provide key improvements in the understanding of fuel consumption and heating of nearby surfaces. Practical applications that rely on this include wildfire propagation in wind-driven scenarios, and diffusion flame engineering setups.
横流扰动对层流边界层火焰中条纹的影响
本文采用直接数值模拟的方法,分析了层流边界层火焰中条纹在三种横流扰动状态下的动力学特性:无扰动、受自由流湍流扰动(0.03%≤TI≤1%)和受稳态正弦模拟人造条纹扰动。模拟表明,条纹行为高度依赖于扰动状态。未受扰动的横流导致条纹延迟出现,并产生较小的不稳定的蜿蜒条纹。在这些条件下,由于条纹振幅小,火焰下方表面的热通量保持均匀。自由流湍流使火焰起爆时间提前,条纹波数增加,火焰表面扰动幅度增大。当TI≥0.6%时,条纹生长速率符合典型的瑞利-泰勒不稳定性的二次标度,但当TI较低时,条纹的不稳定性振幅仍然在线性稳定性理论标度控制下生长。稳定的正弦扰动可以用来控制生成的条纹的数量,这些条纹与横流速度谷对齐。对于低波数正弦扰动(k<4),较大的准稳定条纹与较小的非定常蜿蜒条纹重叠。较大的正弦扰动波数(k≥4)诱导出较大的稳定条纹,这些条纹分离成手指状结构,在其中燃料包被带到下游,燃烧继续进行。这对估计底表面的热通量有很大的影响,由于槽下火焰距离较低,最初的热通量更强,但一旦手指状结构发展起来,情况就相反了。新颖性和意义声明边界层火焰在很大程度上是一种尚未开发的反应流动装置,特别是在层流状态下。本研究首次模拟了层流边界层火焰,解决了横流扰动状态对条纹发育和生长的影响,这是以往实验研究文献的主要空白。结果证实了瑞利-泰勒不稳定性的存在,并表明所引入的扰动决定了扰动生长和波数,并极大地影响了附近表面的热通量。揭示的基本物理见解为理解燃料消耗和附近表面的加热提供了关键的改进。依赖于此的实际应用包括风力驱动场景下的野火传播,以及扩散火焰工程设置。
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
Combustion and Flame
Combustion and Flame 工程技术-工程:化工
CiteScore
9.50
自引率
20.50%
发文量
631
审稿时长
3.8 months
期刊介绍: The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on: Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including: Conventional, alternative and surrogate fuels; Pollutants; Particulate and aerosol formation and abatement; Heterogeneous processes. Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including: Premixed and non-premixed flames; Ignition and extinction phenomena; Flame propagation; Flame structure; Instabilities and swirl; Flame spread; Multi-phase reactants. Advances in diagnostic and computational methods in combustion, including: Measurement and simulation of scalar and vector properties; Novel techniques; State-of-the art applications. Fundamental investigations of combustion technologies and systems, including: Internal combustion engines; Gas turbines; Small- and large-scale stationary combustion and power generation; Catalytic combustion; Combustion synthesis; Combustion under extreme conditions; New concepts.
×
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:604180095
Book学术官方微信
小红书