Experimental investigation of NH3-H2 jet flames adopting multi-scalar imaging: Comparison of turbulent burning velocities obtained using different flame-front markers
Ze Wang , Xun Li , Tao Li , Andreas Dreizler , Seyed M. Mousavi , Andrei N. Lipatnikov , Bo Zhou
{"title":"Experimental investigation of NH3-H2 jet flames adopting multi-scalar imaging: Comparison of turbulent burning velocities obtained using different flame-front markers","authors":"Ze Wang , Xun Li , Tao Li , Andreas Dreizler , Seyed M. Mousavi , Andrei N. Lipatnikov , Bo Zhou","doi":"10.1016/j.combustflame.2025.114054","DOIUrl":null,"url":null,"abstract":"<div><div>A series of lean NH<sub>3</sub>/H<sub>2</sub>/O<sub>2</sub>/N<sub>2</sub> pilot jet flames is investigated using simultaneous planar laser-induced fluorescence (PLIF) imaging of NH<sub>3</sub>/NH/OH species. Turbulent rms velocity <span><math><mrow><mo>(</mo><msup><mi>u</mi><mo>′</mo></msup><mo>)</mo></mrow></math></span> and Karlovitz number <span><math><mrow><mo>(</mo><mrow><mi>K</mi><mi>a</mi></mrow><mo>)</mo></mrow></math></span> are varied in a wide range by changing the inlet bulk flow velocity. 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 and Karlovitz number are varied in a wide range by changing the inlet bulk flow velocity. The Lewis number is varied by changing the hydrogen volume fraction in the fuel blends. Laminar flame speed , flame thickness , and Zel'dovich number are varied by enriching air with oxygen. Turbulent burning velocities 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 , which is associated with an isosurface within flame preheat zones, is weakly affected by variations in or , the three other burning velocities, which are associated with isosurfaces within flame reaction zones, are significantly higher in flames characterized by smaller or . Third, for NH and OH marked flame fronts, the increase in with decreasing is attributed to differential diffusion effects, which are more pronounced for NH3/H2/air mixtures characterized by a higher when compared to the counterpart mixtures enriched with oxygen. Fourth, the data measured at the highest and do not show any sign of levelling-off of -curves but imply significant influence of differential diffusion on (for NH and OH isosurfaces). Fifth, the experimental data on can be well approximated using power-law fits with respect to and and substituting major characteristics of unperturbed laminar flames, i.e., and , 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 are quantified using areas of mean isoscalar contours associated with these species and are compared with one another. Whie is insensitive to variations in laminar flame thickness or Lewis number, the other burning velocities are significantly increased with decreasing the thickness or . 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 at Karlovitz numbers as high as 1670 and are well approximated within the framework of leading point concept.
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