Experimental investigation of NH3-H2 jet flames adopting multi-scalar imaging: Comparison of turbulent burning velocities obtained using different flame-front markers

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS
Ze Wang , Xun Li , Tao Li , Andreas Dreizler , Seyed M. Mousavi , Andrei N. Lipatnikov , Bo Zhou
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The Lewis number <span><math><mrow><mo>(</mo><mrow><mi>L</mi><mi>e</mi></mrow><mo>)</mo></mrow></math></span> is varied by changing the hydrogen volume fraction in the fuel blends. Laminar flame speed <span><math><mrow><mo>(</mo><msub><mi>S</mi><mi>L</mi></msub><mo>)</mo></mrow></math></span>, flame thickness <span><math><mrow><mo>(</mo><msub><mi>δ</mi><mi>L</mi></msub><mo>)</mo></mrow></math></span>, and Zel'dovich number <span><math><mrow><mo>(</mo><mrow><mi>Z</mi><mi>e</mi></mrow><mo>)</mo></mrow></math></span> are varied by enriching air with oxygen. Turbulent burning velocities <span><math><mrow><mo>(</mo><msub><mi>U</mi><mi>T</mi></msub><mo>)</mo></mrow></math></span> are evaluated by measuring the inlet mass flow rates and mean flame front areas associated with different flame markers, i.e., NH<sub>3</sub>, NH, and OH. The obtained results show the following trends. First, there are significant quantitative differences between burning velocities measured using different flame front markers. Second, while <span><math><msub><mi>U</mi><mrow><mi>T</mi><mo>,</mo><mtext>NH</mtext><mn>3</mn></mrow></msub></math></span>, which is associated with an isosurface within flame preheat zones, is weakly affected by variations in <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span> or <span><math><msub><mi>δ</mi><mi>L</mi></msub></math></span>, the three other burning velocities, which are associated with isosurfaces within flame reaction zones, are significantly higher in flames characterized by smaller <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span> or <span><math><msub><mi>δ</mi><mi>L</mi></msub></math></span>. Third, for NH and OH marked flame fronts, the increase in <span><math><msub><mi>U</mi><mi>T</mi></msub></math></span> with decreasing <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span> is attributed to differential diffusion effects, which are more pronounced for NH<sub>3</sub>/H<sub>2</sub>/air mixtures characterized by a higher <span><math><mrow><mi>Z</mi><mi>e</mi></mrow></math></span> when compared to the counterpart mixtures enriched with oxygen. Fourth, the data measured at the highest <span><math><mrow><msup><mi>u</mi><mo>′</mo></msup><mo>/</mo><msub><mi>S</mi><mi>L</mi></msub><mo>=</mo><mn>234</mn></mrow></math></span> and <span><math><mrow><mi>K</mi><mi>a</mi><mo>=</mo><mn>1670</mn></mrow></math></span> do not show any sign of levelling-off of <span><math><mrow><msub><mi>U</mi><mi>T</mi></msub><mrow><mo>(</mo><msup><mi>u</mi><mo>′</mo></msup><mo>)</mo></mrow></mrow></math></span>-curves but imply significant influence of differential diffusion on <span><math><msub><mi>U</mi><mi>T</mi></msub></math></span> (for NH and OH isosurfaces). Fifth, the experimental data on <span><math><mrow><msub><mi>U</mi><mi>T</mi></msub><mo>/</mo><msub><mi>S</mi><mi>L</mi></msub></mrow></math></span> can be well approximated using power-law fits with respect to <span><math><mrow><msup><mi>u</mi><mo>′</mo></msup><mo>/</mo><msub><mi>S</mi><mi>L</mi></msub></mrow></math></span> and <span><math><mrow><mi>L</mi><mo>/</mo><msub><mi>δ</mi><mi>L</mi></msub></mrow></math></span> and substituting major characteristics of unperturbed laminar flames, i.e., <span><math><msub><mi>S</mi><mi>L</mi></msub></math></span> and <span><math><msub><mi>δ</mi><mi>L</mi></msub></math></span>, with the counterpart characteristics of highly strained laminar flames. This finding supports leading point concept of premixed turbulent combustion.</div></div><div><h3>Novelty and Significance Statement</h3><div>Three different species (NH<sub>3</sub>, NH, and OH) are simultaneously measured in lean NH<sub>3</sub>/H<sub>2</sub>/O<sub>2</sub>/N<sub>2</sub> turbulent jet flames adapting two aligned laser diagnostics systems. Turbulent burning velocities <span><math><msub><mi>U</mi><mi>T</mi></msub></math></span> are quantified using areas of mean isoscalar contours associated with these species and are compared with one another. Whie <span><math><msub><mi>U</mi><mrow><mi>T</mi><mo>,</mo><mtext>NH</mtext><mn>3</mn></mrow></msub></math></span> is insensitive to variations in laminar flame thickness or Lewis number, the other burning velocities are significantly increased with decreasing the thickness or <span><math><mrow><mi>L</mi><mi>e</mi></mrow></math></span>. These measured results imply, for the first time to the authors’ knowledge, qualitatively different behaviors of turbulent burning velocities associated with flame preheat (NH<sub>3</sub>) and reaction (NH and OH) zones. Moreover, the experimental data indicate a significant influence of differential diffusion on <span><math><msub><mi>U</mi><mi>T</mi></msub></math></span> at Karlovitz numbers as high as 1670 and are well approximated within the framework of leading point concept.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"275 ","pages":"Article 114054"},"PeriodicalIF":5.8000,"publicationDate":"2025-02-27","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/S0010218025000926","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0

Abstract

A series of lean NH3/H2/O2/N2 pilot jet flames is investigated using simultaneous planar laser-induced fluorescence (PLIF) imaging of NH3/NH/OH species. Turbulent rms velocity (u) and Karlovitz number (Ka) are varied in a wide range by changing the inlet bulk flow velocity. The Lewis number (Le) is varied by changing the hydrogen volume fraction in the fuel blends. Laminar flame speed (SL), flame thickness (δL), and Zel'dovich number (Ze) are varied by enriching air with oxygen. Turbulent burning velocities (UT) are evaluated by measuring the inlet mass flow rates and mean flame front areas associated with different flame markers, i.e., NH3, NH, and OH. The obtained results show the following trends. First, there are significant quantitative differences between burning velocities measured using different flame front markers. Second, while UT,NH3, which is associated with an isosurface within flame preheat zones, is weakly affected by variations in Le or δL, the three other burning velocities, which are associated with isosurfaces within flame reaction zones, are significantly higher in flames characterized by smaller Le or δL. Third, for NH and OH marked flame fronts, the increase in UT with decreasing Le is attributed to differential diffusion effects, which are more pronounced for NH3/H2/air mixtures characterized by a higher Ze when compared to the counterpart mixtures enriched with oxygen. Fourth, the data measured at the highest u/SL=234 and Ka=1670 do not show any sign of levelling-off of UT(u)-curves but imply significant influence of differential diffusion on UT (for NH and OH isosurfaces). Fifth, the experimental data on UT/SL can be well approximated using power-law fits with respect to u/SL and L/δL and substituting major characteristics of unperturbed laminar flames, i.e., SL and δL, with the counterpart characteristics of highly strained laminar flames. This finding supports leading point concept of premixed turbulent combustion.

Novelty and Significance Statement

Three different species (NH3, NH, and OH) are simultaneously measured in lean NH3/H2/O2/N2 turbulent jet flames adapting two aligned laser diagnostics systems. Turbulent burning velocities UT are quantified using areas of mean isoscalar contours associated with these species and are compared with one another. Whie UT,NH3 is insensitive to variations in laminar flame thickness or Lewis number, the other burning velocities are significantly increased with decreasing the thickness or Le. These measured results imply, for the first time to the authors’ knowledge, qualitatively different behaviors of turbulent burning velocities associated with flame preheat (NH3) and reaction (NH and OH) zones. Moreover, the experimental data indicate a significant influence of differential diffusion on UT at Karlovitz numbers as high as 1670 and are well approximated within the framework of leading point concept.
采用多标量成像的NH3-H2射流火焰实验研究:不同火焰前标记得到的湍流燃烧速度的比较
利用同步平面激光诱导荧光(PLIF)成像技术研究了一系列贫NH3/H2/O2/N2先导射流火焰。湍流均方根速度(u’)和卡洛维茨数(Ka)随着进口体流速度的改变而有较大的变化。路易斯数(Le)是通过改变燃料混合物中氢体积分数而改变的。层流火焰速度(SL)、火焰厚度(δL)和泽尔多维奇数(Ze)随着空气中氧气的富集而变化。湍流燃烧速度(UT)通过测量入口质量流量和与不同火焰标记物(即NH3, nhh和OH)相关的平均火焰前面积来评估。所得结果显示如下趋势。首先,使用不同火焰前标记物测量的燃烧速度之间存在显著的数量差异。其次,与火焰预热区等面相关的UT、NH3受Le或δL变化的影响较小,而与火焰反应区等面相关的其他三种燃烧速度在Le或δL较小的火焰中明显更高。第三,对于NH和OH标记的火焰锋面,随着Le的降低,UT的增加归因于扩散效应的差异,与富氧的对应混合物相比,具有较高Ze的NH3/H2/空气混合物的扩散效应更为明显。第四,在最高u′/SL=234和Ka=1670处测量的数据没有显示UT(u′)曲线趋于平缓的迹象,但表明微分扩散对UT(对于nhh和OH等面)有显著影响。第五,利用u′/SL和L/δL的幂律拟合,将无扰动层流火焰的主要特征,即SL和δL替换为高应变层流火焰的对应特征,可以很好地逼近UT/SL的实验数据。这一发现支持了预混湍流燃烧的先导点概念。新新性和意义声明采用两台对齐的激光诊断系统,在稀薄的NH3/H2/O2/N2湍流射流火焰中同时测量了三种不同的物质(NH3, nhh和OH)。湍流燃烧速度UT使用与这些物种相关的平均等标量等高线的面积进行量化,并相互比较。而UT、NH3对层流火焰厚度和Lewis数的变化不敏感,其他燃烧速度随层流火焰厚度和Lewis数的减小而显著增加。据作者所知,这些测量结果首次表明,湍流燃烧速度与火焰预热区(NH3)和反应区(NH和OH)相关的性质不同。此外,实验数据表明,在Karlovitz数高达1670时,微分扩散对UT有显著的影响,并且在先导点概念的框架内可以很好地近似。
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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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