H2/N2湍流火焰的拉曼-瑞利和lifoh测量

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS
A.R.W. Macfarlane , H. Tang , M.J. Dunn , G. Magnotti , A.R. Masri
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引用次数: 0

摘要

本文介绍了利用拉曼/瑞利散射在H2/N2 = 40/60体积的湍流部分预混火焰中进行的温度和物质测量,这些火焰来自悉尼非均匀驾驶喷气燃烧器。报道了等效比为φ = 4.76的三个火焰的结果,其中一个火焰的入口成分不均匀,在吹出速度的80%,另两个火焰的入口成分均匀,一个速度等于不均匀火焰,另一个速度等于吹出速度的80%。这项工作的一个关键发现是,使用化学发光和OH平面荧光成像验证,非均匀火焰大约是均匀火焰长度的一半。对O2、N2、H2O和H2的温度和质量分数的测量表明,三种火焰在混合、反应性和微分扩散方面存在显著差异,特别是在出口附近。在成分不均匀的情况下,在出口处有大量未反应和部分反应的燃料,这是由于环空空气与射流中的燃料之间的凹槽距离短,速度比大。这些可能分层的不均匀混合物与热先导产物相互作用,并表现出显著的应变速率,从而局部消失。在两种均匀情况下,火焰在射流出口附近燃烧强劲,只有在较高的射流速度下局部熄灭略有增加。低速均匀火焰在出口附近具有明显的微分扩散,类似于低应变多分量火焰。而非均匀和高速均匀火焰都具有最小的微分扩散,分别非常类似于高应变多分量和单位路易斯数火焰模拟。对于这三种火焰,混合物的分数、温度和物质分布接近于相似的下游标量分布,反映了局部消光和微分扩散效应的衰减。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Raman-Rayleigh and LIF-OH measurements in turbulent H2/N2 flames with and without compositional inhomogeneity
This paper presents temperature and species measurements performed using Raman/Rayleigh scattering in turbulent partially premixed flames of H2/N2 = 40/60 by volume, issuing from the Sydney inhomogeneous piloted jet burner. Results are reported for three flames, with an equivalence ratio of φ = 4.76, one with a compositional inhomogeneous inlet, at 80 % of the blow-off velocity and the other two flames being compositionally homogeneous, one velocity is equal to the inhomgoeneous flame and the other at 80 % from blow-off. A key finding of this work is that the inhomogeneous flame is approximately half the length of the homogeneous flames, as verified using chemiluminescence and OH planar fluorescence imaging. Measurements of temperature and mass fractions of O2, N2, H2O and H2 reveal significant differences in the mixing, reactivity and differential diffusion between the three flames, particularly near the outlet. For the compositionally inhomogeneous case, there is a significant amount of unreacted and partially reacted fuel, at the outlet, and this is due to the short recess distance and large velocity ratio between the air in the annulus and fuel in the jet. These inhomogeneous mixtures, which may be stratified, interact with the hot pilot products and exhibit significant strain rates and hence local extinction. For both homogeneous cases, the flame burns robustly near the jet exit with only a modest increase in local extinction at higher jet velocities. The low velocity homogeneous flame has significant differntial diffusion close to the outlet, resembling a low strained multicomponent flamelet. Whilst both the inhomogeneous and high-velocity homogeneous flames have minimal differential diffusion, closely resemblimg a highly strained mutlicomponent and unity Lewis number flamelet simulation respectively. For all three flames, the mixture fraction, temperature, and species profiles approach similar scalar profiles downstream, reflecting a decay in the local extinction and differential diffusion effects.
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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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