评估热扩散贫油预混 H2/空气火焰的湍流-火焰相互作用,以实现分布式燃烧机制

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Combustion and Flame Pub Date : 2024-09-02 DOI:10.1016/j.combustflame.2024.113699
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The same combustion diagnostics are applied to another lean premixed hydrogen/air turbulent flame with an initial equivalence ratio of 0.4 and a bulk velocity of 200<!--> <!-->m/s at selected downstream locations of <span><math><mrow><mi>x</mi><mo>/</mo><mi>D</mi></mrow></math></span> <!--> <!-->=<!--> <!-->3.5, 7, 10.5, and 14 to assess the effects of developing turbulence and residence time. Corresponding Karlovitz numbers are 680, 730, 775, and 690, as the local turbulent intensity changes along downstream locations. While flame structures reveal characteristics towards distributed burning at lower <span><math><mrow><mi>x</mi><mo>/</mo><mi>D</mi></mrow></math></span>, a locally intense burning region appears at higher <span><math><mrow><mi>x</mi><mo>/</mo><mi>D</mi></mrow></math></span> together with positive curvature. 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引用次数: 0

摘要

利用激光诱导 OH 自由基荧光和粒子图像测速同时测量法,以及准同时一维拉曼/瑞利散射和二维瑞利散射测量法,研究了卡尔洛维茨数(通过改变等效比)和停留时间(通过改变轴向测量位置)对贫氢气/空气预混合湍流喷射火焰内部火焰结构的影响。讨论了在 100 米/秒的恒定体积速度下,一组初始当量比分别为 0.3、0.4 和 0.45 的贫油预混氢气/空气湍流火焰的湍流流场、瞬时宏观火焰结构和热化学状态。随着当量比的增加,在 x/D = 7 的下游位置测定的湍流场得出的卡尔洛维茨数从 7690 快速下降到 260 和 100。在最高的卡尔洛维茨数(即最低的等效比)下,由于湍流传输比分子混合占优势,且差分扩散和火焰曲率的影响被抑制,因此在喷射火焰中观察到分布式燃烧。随着卡尔洛维茨数的降低,观察到以局部当量比升高、高水分子分数和超绝热火焰温度为特征的剧烈燃烧区域,并伴有正火焰曲率。在选定的下游位置 x/D = 3.5、7、10.5 和 14 处,对初始当量比为 0.4、体积速度为 200 米/秒的另一种贫油预混氢气/空气湍流火焰进行了相同的燃烧诊断,以评估发展湍流和停留时间的影响。随着下游位置局部湍流强度的变化,相应的卡尔洛维茨数分别为 680、730、775 和 690。在较低的 x/D 值下,火焰结构显示出分布式燃烧的特点,而在较高的 x/D 值下,则会出现局部剧烈燃烧区域,并伴有正曲率。这主要是因为湍流随着 x/D 的增大而发展,随着湍流长度尺度的增大,火焰表面受湍流涡的扰动和弯曲程度增大。高度扩散的氢气被正弯曲的火焰表面局部集中,从而形成温度较高的富燃料燃烧区。这表明,随着轴向速度波动的增加,湍流也会在一定程度上促进热扩散不稳定性,通过与常压下氢气的差分扩散效应相互作用,增加混合物在温度空间的不均匀性。对包括氢气/空气喷射火焰的湍流场(粒子图像测速仪)、瞬时火焰结构(OH 自由基的激光诱导荧光)和内部热化学状态(准同步一维拉曼/瑞利和二维瑞利散射成像)在内的综合实验结果进行了分析和讨论。数据集具有良好的边界条件和较高的测量精度,对于验证和开发数值模拟模型至关重要。
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Assessing turbulence–flame interaction of thermo-diffusive lean premixed H2/air flames towards distributed burning regime

Simultaneous laser-induced fluorescence of OH radicals and particle image velocimetry, and quasi-simultaneous 1D Raman/Rayleigh and 2D Rayleigh scattering measurements are used to investigate the effects of Karlovitz number (by varying the equivalence ratio) and residence time (by varying the axial measurement location) on the internal flame structures of lean premixed hydrogen/air turbulent jet flames. The turbulent flow fields, instantaneous macroscopic flame structures, and thermochemical states of a set of lean premixed hydrogen/air turbulent flames with varying initial equivalence ratio of 0.3, 0.4, and 0.45 at a constant bulk velocity of 100 m/s are discussed. With an increasing equivalence ratio, the Karlovitz number derived from the turbulent flow fields decreases rapidly from 7690 to 260 and 100, determined at a downstream location of x/D  = 7. At the highest Karlovitz number (i.e., the lowest equivalence ratio), a distributed burning is observed in the jet flame as turbulent transport dominates over molecular mixing, and the effects of differential diffusion and flame curvature are suppressed. With decreasing Karlovitz number, intense burning regions characterized by elevated local equivalence ratio, high water mole fraction, and super-adiabatic flame temperatures are observed in association with positive flame curvature. The same combustion diagnostics are applied to another lean premixed hydrogen/air turbulent flame with an initial equivalence ratio of 0.4 and a bulk velocity of 200 m/s at selected downstream locations of x/D  = 3.5, 7, 10.5, and 14 to assess the effects of developing turbulence and residence time. Corresponding Karlovitz numbers are 680, 730, 775, and 690, as the local turbulent intensity changes along downstream locations. While flame structures reveal characteristics towards distributed burning at lower x/D, a locally intense burning region appears at higher x/D together with positive curvature. This is mainly because the turbulence develops with increasing x/D and the flame surface is more disturbed and curved by turbulent eddies with increasing turbulence length scales. The highly diffusive hydrogen is locally concentrated by positively curved flame surfaces, resulting in fuel-rich burning regions at a higher temperature. This indicates that, as velocity fluctuations increase in axial direction, turbulence can also promote thermo-diffusive instabilities to a certain extent, increasing the mixture inhomogeneity in temperature space by interacting with the differential diffusion effect of hydrogen at atmospheric pressure.

Novelty and significance

The novelty of the current work is the focus on turbulence–chemistry interactions of premixed hydrogen/air jet flames at high turbulence and ultra lean conditions. Comprehensive experimental results including the turbulent flow fields (particle image velocimetry), instantaneous flame structures (laser-induced fluorescence of OH radicals) and internal thermochemical states (quasi-simultaneous 1D Raman/Rayleigh and 2D Rayleigh scattering imaging) of hydrogen/air jet flames are analyzed and discussed. The data sets with well-characterized boundary conditions and high measurement accuracy, are crucial for validation and development of numerical simulation models.

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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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