Combined effects of heat losses and curvature in hydrogen–air flame propagation below the lean flammability limit

IF 4.6 2区 工程技术 Q2 ENERGY & FUELS
Proceedings of the Combustion Institute Pub Date : 2026-01-01 Epub Date: 2026-06-29 DOI:10.1016/j.proci.2026.106100
Rubén Palomeque-Santiago, Anne Dejoan, Daniel Fernández-Galisteo, Mariano Rubio-Rubio, Mario Sánchez-Sanz
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引用次数: 0

Abstract

Recent experiments have shown that, below the flammability limit, ultra-lean hydrogen flame fronts can fragment into isolated flame cells when propagating within narrow channels. To further elucidate the underlying mechanisms of this behavior, three-dimensional (3D) numerical simulations are performed, systematically varying the heat losses through the confining walls. Under adiabatic conditions, a continuous flame front embedded with small cellular structures is sustained. When heat losses are introduced, this front fragments, forming isolated flame cells. The characteristic size of these cells is found to be comparable to the dominant wavelength of the corrugated front obtained under adiabatic conditions. The results indicate that heat losses have a pronounced impact on the flame curvature between the wall plates, which transitions from a highly asymmetric configuration to a nearly circular shape as the heat losses increase, while the curvature in the mid-channel plane is barely affected. The size and propagation velocity of the isolated flame cells exhibit a moderate dependence on the magnitude of the heat losses. Sufficiently large heat losses induce a bifurcation of the isolated fronts from a circular to a double-cell flame shape
Novelty and significance statement
This work presents fully three-dimensional numerical simulations to investigate the mechanisms governing the fragmentation of ultra-lean hydrogen–air flame fronts in narrow channels under the influence of varying wall heat losses. The main novelty is the quantification of the heat-loss effect on flame curvature, both across and along the confining plates. A direct correspondence is established between the characteristic size of the isolated cells and the dominant wavelength of flame corrugation under adiabatic conditions, revealing how increasing heat losses promote the transition from a non-symmetric flame to stable, symmetric isolated flame cells below the lean flammability limit of the adiabatic planar deflagration. This study explains that heat losses, typically associated with quenching, can instead stabilize discrete flame cells by reshaping the flame’s three-dimensional curvature and propagation dynamics. These findings clarify the mechanisms behind stable ultra-lean hydrogen combustion, with direct implications for hydrogen safety and the design of efficient, low-emission micro-combustion systems.
低可燃性极限下氢气-空气火焰传播过程中热损失和曲率的综合影响
最近的实验表明,在可燃性极限以下,超贫氢火焰锋面在狭窄通道内传播时可以破碎成孤立的火焰细胞。为了进一步阐明这种行为的潜在机制,进行了三维(3D)数值模拟,系统地改变了通过围壁的热损失。在绝热条件下,一个嵌有小胞状结构的连续火焰前缘得以维持。当热损失被引入时,这个锋面破碎,形成孤立的火焰细胞。发现这些细胞的特征尺寸与绝热条件下获得的波纹锋的主波长相当。结果表明:热损失对壁板间的火焰曲率有显著影响,随着热损失的增加,壁板间的火焰曲率从高度不对称的形状转变为近似圆形的形状,而通道中平面的曲率几乎没有受到影响。孤立火焰细胞的大小和传播速度表现出适度依赖于热损失的大小。足够大的热损失导致孤立锋面从圆形火焰形状分叉为双室火焰形状。本文提出了完全三维数值模拟,以研究在不同壁面热损失的影响下,狭窄通道中超贫氢-空气火焰锋面破碎的机制。主要的新颖之处是量化热损失对火焰曲率的影响,包括围板两侧和围板两侧。在绝热条件下,隔离室的特征尺寸与火焰波纹的主要波长之间建立了直接对应关系,揭示了热损失的增加如何促进从非对称火焰过渡到稳定的对称隔离焰室,其可燃性低于绝热平面燃速的低可燃性极限。这项研究解释了通常与淬火相关的热损失可以通过重塑火焰的三维曲率和传播动力学来稳定离散的火焰细胞。这些发现阐明了稳定的超贫氢燃烧背后的机制,对氢的安全性和高效、低排放微燃烧系统的设计具有直接意义。
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来源期刊
Proceedings of the Combustion Institute
Proceedings of the Combustion Institute 工程技术-工程:化工
CiteScore
7.00
自引率
0.00%
发文量
420
审稿时长
3.0 months
期刊介绍: The Proceedings of the Combustion Institute contains forefront contributions in fundamentals and applications of combustion science. For more than 50 years, the Combustion Institute has served as the peak international society for dissemination of scientific and technical research in the combustion field. In addition to author submissions, the Proceedings of the Combustion Institute includes the Institute''s prestigious invited strategic and topical reviews that represent indispensable resources for emergent research in the field. All papers are subjected to rigorous peer review. Research papers and invited topical reviews; Reaction Kinetics; Soot, PAH, and other large molecules; Diagnostics; Laminar Flames; Turbulent Flames; Heterogeneous Combustion; Spray and Droplet Combustion; Detonations, Explosions & Supersonic Combustion; Fire Research; Stationary Combustion Systems; IC Engine and Gas Turbine Combustion; New Technology Concepts The electronic version of Proceedings of the Combustion Institute contains supplemental material such as reaction mechanisms, illustrating movies, and other data.
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