The measurement of turbulent burning velocities of methane-hydrogen-air mixtures at elevated pressures in a spherical vessel

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS Combustion and Flame Pub Date : 2025-02-01 Epub Date: 2024-12-14 DOI:10.1016/j.combustflame.2024.113907
Marwaan Al-Khafaji , Junfeng Yang , Alison S. Tomlin , Harvey M. Thompson , Gregory de Boer , Kexin Liu
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Abstract

Few previous experimental studies have focused on pre-mixed turbulent burning velocities (ut) for hydrogen/air and methane/hydrogen/air mixtures, especially at the high-pressure conditions most relevant to gas turbine applications. This work employed a Schlieren technique to measure flame speeds for such mixtures in a spherical stainless steel combustion vessel, from which turbulent burning velocities were derived. The hydrogen volume fractions in methane were 30, 50, 70 and 100%. The initial pressures were 0.1, 0.5 and 1.0 MPa, and the initial temperatures were 303 and 360 K. The equivalence ratio (ϕ) was varied between 0.5 and 2 for pure hydrogen and from 0.8 to 1.2 for methane/hydrogen mixtures. The root mean square (rms) turbulent velocity (u’) was varied from 2.0 to 10.0 ms−1. The objectives of this study are: (a) to present an extensive experimental database of turbulent burning velocities for these mixtures over a wide range of conditions; (b) to establish a new correlation for ut for a flame with Lewis numbers, Le, not equal to unity, and (c) to quantify the dependence of turbulent burning velocity on pressure, temperature, stretch rate, laminar flame instability and rms velocity. As the pressure increased, the Taylor length scales decreased, and positive stretch increased, increasing flame wrinkling and ut. The ut also increased as the temperature and u’ increased. The fuel/air mixture with high laminar flame instability (Le<1) has higher ut than those with higher Le. However, the normalised ut peaked in the region of high laminar burning velocity. This study concluded that the increase in ut resulting from flame reactivity (laminar burning velocity) is more important than that from positive stretch (negative Mab) and flame instability.
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在球形容器中测量甲烷-氢-空气混合物在高压下的湍流燃烧速度
以前很少有实验研究关注氢气/空气和甲烷/氢气/空气混合物的预混合湍流燃烧速度(ut),特别是在与燃气轮机应用最相关的高压条件下。这项工作采用纹影技术在一个球形不锈钢燃烧容器中测量这种混合物的火焰速度,并由此得出湍流燃烧速度。氢气在甲烷中的体积分数分别为30%、50%、70%和100%。初始压力分别为0.1、0.5和1.0 MPa,初始温度分别为303和360 K。等效比(φ)变化在0.5和2之间的纯氢和0.8至1.2之间的甲烷/氢混合物。湍流速度(u ')的均方根(rms)变化范围为2.0 ~ 10.0 ms−1。本研究的目的是:(a)在广泛的条件下,为这些混合物提供一个广泛的湍流燃烧速度的实验数据库;(b)建立新的火焰燃烧速度与刘易斯数Le不等于单位的相关性;(c)量化湍流燃烧速度对压力、温度、拉伸率、层流火焰不稳定性和均方根速度的依赖关系。随着压力的增加,泰勒长度尺度减小,正拉伸增大,火焰起皱和厚度增大。ut随温度和u′的升高而增大。具有高层流火焰不稳定性(Le<1)的燃料/空气混合物比具有高Le<;1的燃料/空气混合物具有更高的ut。然而,归一化温度在层流燃烧速度高的区域达到峰值。该研究得出结论,火焰反应性(层流燃烧速度)导致的ut增加比正拉伸(负Mab)和火焰不稳定性更重要。
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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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