适应非统一路易斯数混合物弱拉伸火焰的加厚火焰模型

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Combustion and Flame Pub Date : 2024-10-10 DOI:10.1016/j.combustflame.2024.113758
S. Poncet, C. Mehl, K. Truffin, O. Colin
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However, when considering differential diffusion effects, the modification of flame reactivity induced by strain rate and curvature is enhanced by the flame thickening process. Especially, at low stretch rates, the derivative of the flame speed with stretch, i.e. the Markstein length <span><math><mi>L</mi></math></span>, is multiplied by <span><math><mi>F</mi></math></span>. This induces large errors on the stretched flame speed estimation for mixtures with Lewis numbers <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span> far from unity, such as for lean hydrogen/air combustion. The present work proposes a methodology to recover the exact Markstein length of thickened flames, called <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM. This easy-to-implement method relies on a 2-parameters evaluation, which monitors <span><math><mi>L</mi></math></span> and <span><math><msubsup><mrow><mi>S</mi></mrow><mrow><mi>L</mi></mrow><mrow><mn>0</mn></mrow></msubsup></math></span>. Various Markstein length definitions from literature are considered and estimated using two laminar stretched flame configurations: (i) reactants-to-products counter-flow and (ii) spherical flames. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is evaluated for (i) lean H<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span>/air (<span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span>) and (ii) stoichiometric C<span><math><msub><mrow></mrow><mrow><mn>8</mn></mrow></msub></math></span>H<sub>18</sub>/air (<span><math><mrow><mi>L</mi><mi>e</mi><mo>&gt;</mo><mn>1</mn></mrow></math></span>) mixtures at ambient conditions. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM accurately recovers the targeted Markstein lengths for both mixtures, enabling precise estimation of either consumption or displacement flame speed at low stretch rates. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM remains fairly accurate even at large strain rates for the <span><math><mrow><mi>L</mi><mi>e</mi><mo>&gt;</mo><mn>1</mn></mrow></math></span> flame, while on the contrary for the <span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span> flame, the consumption speed is highly under-predicted. The extinction strain rate with <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is then assessed, showing a systematic under-prediction of the extinction strain rate for both flames, as with standard TFM. Additional work is thus needed to shed light on <span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span> flame conditions. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is finally evaluated on a flame-vortex configuration with the stoichiometric C<span><math><msub><mrow></mrow><mrow><mn>8</mn></mrow></msub></math></span>H<sub>18</sub>/air mixture. The evolution of flame geometry and flame front reactivity are both better estimated with <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM than with standard TFM.</div><div><strong>Novelty and Significance Statement</strong></div><div>This paper presents a novel method to correct the over-sensitivity of the Thickened Flame Model to low stretch rates by adjusting the species diffusivities and reaction rates via two multiplicative parameters. While previous studies only considered counter-flow strained flames to establish their model parameters, this study assesses the impact of the canonical flame configuration employed by comparing strained and curved (spherical) flames. The choice of the laminar flame speed considered (consumption or displacement speed) is also assessed for the first time. Most importantly, while previous stretch correction methods were applied exclusively on positive Markstein length mixtures (<span><math><mrow><mi>L</mi><mi>e</mi><mo>&gt;</mo><mn>1</mn></mrow></math></span> cases), it is shown that the proposed stretch correction can be applied to negative Markstein length mixtures as well (here a lean H<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span>/air mixture), provided the stretch rate remains low. Finally, as a first step towards flame/turbulence interaction modeling, the stretch correction efficiency is quantified for the first time on a canonical flame-vortex configuration.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"270 ","pages":"Article 113758"},"PeriodicalIF":5.8000,"publicationDate":"2024-10-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A Thickened Flame Model adaptation to weakly stretched flames for non-unity Lewis number mixtures\",\"authors\":\"S. Poncet,&nbsp;C. Mehl,&nbsp;K. Truffin,&nbsp;O. Colin\",\"doi\":\"10.1016/j.combustflame.2024.113758\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>For the study and design of industrial scale combustion systems, the Thickened Flame Model (TFM) is a widely used turbulent combustion model. It allows for the direct resolution of the flame front on Large Eddy Simulation (LES) meshes by artificially thickening the flame front by a factor <span><math><mi>F</mi></math></span>, i.e. <span><math><mrow><msub><mrow><mi>δ</mi></mrow><mrow><mi>L</mi></mrow></msub><mo>=</mo><mi>F</mi><msubsup><mrow><mi>δ</mi></mrow><mrow><mi>L</mi></mrow><mrow><mn>0</mn></mrow></msubsup></mrow></math></span>, while the unstretched adiabatic flame speed <span><math><msubsup><mrow><mi>S</mi></mrow><mrow><mi>L</mi></mrow><mrow><mn>0</mn></mrow></msubsup></math></span> is preserved. However, when considering differential diffusion effects, the modification of flame reactivity induced by strain rate and curvature is enhanced by the flame thickening process. Especially, at low stretch rates, the derivative of the flame speed with stretch, i.e. the Markstein length <span><math><mi>L</mi></math></span>, is multiplied by <span><math><mi>F</mi></math></span>. This induces large errors on the stretched flame speed estimation for mixtures with Lewis numbers <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span> far from unity, such as for lean hydrogen/air combustion. The present work proposes a methodology to recover the exact Markstein length of thickened flames, called <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM. This easy-to-implement method relies on a 2-parameters evaluation, which monitors <span><math><mi>L</mi></math></span> and <span><math><msubsup><mrow><mi>S</mi></mrow><mrow><mi>L</mi></mrow><mrow><mn>0</mn></mrow></msubsup></math></span>. Various Markstein length definitions from literature are considered and estimated using two laminar stretched flame configurations: (i) reactants-to-products counter-flow and (ii) spherical flames. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is evaluated for (i) lean H<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span>/air (<span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span>) and (ii) stoichiometric C<span><math><msub><mrow></mrow><mrow><mn>8</mn></mrow></msub></math></span>H<sub>18</sub>/air (<span><math><mrow><mi>L</mi><mi>e</mi><mo>&gt;</mo><mn>1</mn></mrow></math></span>) mixtures at ambient conditions. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM accurately recovers the targeted Markstein lengths for both mixtures, enabling precise estimation of either consumption or displacement flame speed at low stretch rates. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM remains fairly accurate even at large strain rates for the <span><math><mrow><mi>L</mi><mi>e</mi><mo>&gt;</mo><mn>1</mn></mrow></math></span> flame, while on the contrary for the <span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span> flame, the consumption speed is highly under-predicted. The extinction strain rate with <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is then assessed, showing a systematic under-prediction of the extinction strain rate for both flames, as with standard TFM. Additional work is thus needed to shed light on <span><math><mrow><mi>L</mi><mi>e</mi><mo>&lt;</mo><mn>1</mn></mrow></math></span> flame conditions. <span><math><mrow><mi>M</mi><mi>a</mi></mrow></math></span>-TFM is finally evaluated on a flame-vortex configuration with the stoichiometric C<span><math><msub><mrow></mrow><mrow><mn>8</mn></mrow></msub></math></span>H<sub>18</sub>/air mixture. 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引用次数: 0

摘要

在研究和设计工业规模的燃烧系统时,加厚火焰模型(TFM)是一种广泛使用的湍流燃烧模型。它通过人为地将火焰前沿增厚 F 倍,即 δL=FδL0 来直接解析大涡模拟(LES)网格上的火焰前沿,同时保留未拉伸的绝热火焰速度 SL0。然而,当考虑到差分扩散效应时,应变率和曲率引起的火焰反应性变化会因火焰增粗过程而增强。特别是在低拉伸率时,火焰速度与拉伸的导数(即马克斯坦长度 L)会乘以 F。对于路易斯数 Le 远远低于统一的混合物,例如贫氢/空气燃烧,拉伸火焰速度估算会产生较大误差。本研究提出了一种恢复加厚火焰精确马克斯坦长度的方法,称为 Ma-TFM。这种易于实施的方法依赖于监测 L 和 SL0 的双参数评估。考虑并估算了文献中的各种马克斯坦长度定义,并使用了两种层流拉伸火焰配置:(i) 反应物-生成物逆流和 (ii) 球形火焰。Ma-TFM 针对环境条件下 (i) 贫氢/空气(Le<1)和 (ii) 化学计量 C8H18/空气(Le>1)混合物进行了评估。Ma-TFM 可准确恢复这两种混合物的目标马克斯坦长度,从而在低伸展率条件下精确估算消耗或位移火焰速度。对于 Le>1 火焰,Ma-TFM 即使在较大的应变速率下也能保持相当高的精确度,相反,对于 Le<1 火焰,消耗速度的预测则严重不足。然后对使用 Ma-TFM 的熄灭应变率进行了评估,结果显示,与标准 TFM 一样,两种火焰的熄灭应变率都系统性地预测不足。因此,还需要做更多的工作来揭示 Le<1 火焰条件。Ma-TFM 最后在具有化学计量 C8H18/ 空气混合物的火焰涡流配置上进行了评估。与标准 TFM 相比,Ma-TFM 能更好地估算火焰几何形状的演变和火焰前沿的反应性。以往的研究仅考虑逆流应变火焰来建立模型参数,而本研究通过比较应变火焰和弯曲(球形)火焰来评估所采用的典型火焰配置的影响。此外,还首次评估了所考虑的层流火焰速度(消耗速度或位移速度)的选择。最重要的是,以前的拉伸校正方法只适用于正马克斯坦长度混合物(Le>1 情况),而本文表明,只要拉伸率保持较低水平,建议的拉伸校正方法也可适用于负马克斯坦长度混合物(此处为贫氢/空气混合物)。最后,作为火焰/湍流相互作用建模的第一步,首次对典型火焰-漩涡配置的拉伸修正效率进行了量化。
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A Thickened Flame Model adaptation to weakly stretched flames for non-unity Lewis number mixtures
For the study and design of industrial scale combustion systems, the Thickened Flame Model (TFM) is a widely used turbulent combustion model. It allows for the direct resolution of the flame front on Large Eddy Simulation (LES) meshes by artificially thickening the flame front by a factor F, i.e. δL=FδL0, while the unstretched adiabatic flame speed SL0 is preserved. However, when considering differential diffusion effects, the modification of flame reactivity induced by strain rate and curvature is enhanced by the flame thickening process. Especially, at low stretch rates, the derivative of the flame speed with stretch, i.e. the Markstein length L, is multiplied by F. This induces large errors on the stretched flame speed estimation for mixtures with Lewis numbers Le far from unity, such as for lean hydrogen/air combustion. The present work proposes a methodology to recover the exact Markstein length of thickened flames, called Ma-TFM. This easy-to-implement method relies on a 2-parameters evaluation, which monitors L and SL0. Various Markstein length definitions from literature are considered and estimated using two laminar stretched flame configurations: (i) reactants-to-products counter-flow and (ii) spherical flames. Ma-TFM is evaluated for (i) lean H2/air (Le<1) and (ii) stoichiometric C8H18/air (Le>1) mixtures at ambient conditions. Ma-TFM accurately recovers the targeted Markstein lengths for both mixtures, enabling precise estimation of either consumption or displacement flame speed at low stretch rates. Ma-TFM remains fairly accurate even at large strain rates for the Le>1 flame, while on the contrary for the Le<1 flame, the consumption speed is highly under-predicted. The extinction strain rate with Ma-TFM is then assessed, showing a systematic under-prediction of the extinction strain rate for both flames, as with standard TFM. Additional work is thus needed to shed light on Le<1 flame conditions. Ma-TFM is finally evaluated on a flame-vortex configuration with the stoichiometric C8H18/air mixture. The evolution of flame geometry and flame front reactivity are both better estimated with Ma-TFM than with standard TFM.
Novelty and Significance Statement
This paper presents a novel method to correct the over-sensitivity of the Thickened Flame Model to low stretch rates by adjusting the species diffusivities and reaction rates via two multiplicative parameters. While previous studies only considered counter-flow strained flames to establish their model parameters, this study assesses the impact of the canonical flame configuration employed by comparing strained and curved (spherical) flames. The choice of the laminar flame speed considered (consumption or displacement speed) is also assessed for the first time. Most importantly, while previous stretch correction methods were applied exclusively on positive Markstein length mixtures (Le>1 cases), it is shown that the proposed stretch correction can be applied to negative Markstein length mixtures as well (here a lean H2/air mixture), provided the stretch rate remains low. Finally, as a first step towards flame/turbulence interaction modeling, the stretch correction efficiency is quantified for the first time on a canonical flame-vortex configuration.
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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.
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