Proceedings of the Combustion Institute最新文献_第9页

Influence of magnetic field on flame dynamics in hydrogen flames: A numerical study 磁场对氢火焰火焰动力学影响的数值研究

IF 5.2 2区工程技术 Q2 ENERGY & FUELS

Proceedings of the Combustion Institute

Pub Date : 2025-01-01 DOI: 10.1016/j.proci.2025.105892

Vaibhav Mysore Natesh, Ivan Langella

Electromagnetic fields influence flame behavior by altering the transport of paramagnetic species such as oxygen and OH radicals in hydrogen flames, affecting reaction pathways and combustion dynamics. This study presents a numerical investigation of the effects of magnetic fields on a premixed swirl-stabilized hydrogen flame using a modified combustion solver in OpenFOAM. Additional body force and diffusion terms were incorporated into the governing equations to model interactions with paramagnetic species, and the solver was validated against experimental data and simulations from the literature. The study focuses on analyzing flame structure, species redistribution, and mixture fraction variations under magnetic conditioning. Large Eddy Simulations (LES) with the Eulerian Stochastic Fields (ESF) method were employed to capture turbulence-chemistry interactions. The results indicate that the presence of a magnetic field induces an upstream-directed force on oxygen, leading to localized changes in mixture fraction and combustion characteristics. A reduction in temperature, heat release rate, and OH concentration was observed, with peak reductions of approximately 2%, 5%, and 6%, respectively. These effects are attributed to the redistribution of oxygen, which makes the flame locally leaner. This study extends the understanding of hydrogen combustion under electromagnetic influence and demonstrates the potential of magnetic fields for controlling the flame behavior. The findings provide new insights into magnetic field-assisted combustion strategies, offering a framework for further research in advanced propulsion and energy applications.

电磁场通过改变顺磁性物质如氧和OH自由基在氢火焰中的输运来影响火焰行为，从而影响反应途径和燃烧动力学。本文采用改进的燃烧溶剂在OpenFOAM中对磁场对预混合旋流稳定氢火焰的影响进行了数值研究。在控制方程中加入了额外的体力和扩散项来模拟与顺磁物质的相互作用，并根据实验数据和文献中的模拟对求解器进行了验证。研究重点分析了磁条件下火焰结构、物质重分布和混合分数的变化。采用大涡模拟（LES）和欧拉随机场（ESF）方法捕捉湍流-化学相互作用。结果表明，磁场的存在对氧产生了上游方向的作用力，导致混合气组分和燃烧特性发生局部变化。观察到温度、放热速率和OH浓度的降低，峰值分别降低了约2%、5%和6%。这些影响归因于氧气的再分配，这使得火焰局部变薄。该研究扩展了对电磁影响下氢燃烧的认识，并证明了磁场控制火焰行为的潜力。这一发现为磁场辅助燃烧策略提供了新的见解，为先进推进和能源应用的进一步研究提供了框架。

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引用次数: 0

A priori analysis of multi-dimensional flamelet effects in a transcritical LOX/GH2 jet flame 跨临界LOX/GH2射流火焰中多维火焰效应的先验分析

IF 5.2 2区工程技术 Q2 ENERGY & FUELS

Proceedings of the Combustion Institute

Pub Date : 2025-01-01 DOI: 10.1016/j.proci.2025.105864

Hanzhang Cao, Wang Han, Yihao Tang, Lijun Yang

Accurate modeling of transcritical combustion is of critical importance for the development of high-efficiency rocket engines. While the one-dimensional flamelet theory has been extensively used in transcritical and supercritical combustion simulations, a comprehensive analysis of multi-dimensional flamelet effects remains scarce. To this end, a priori analysis of multi-dimensional flamelet effects in a transcritical LOX/GH2 jet flame is performed in this work by comparing 1D flamelet solutions with multi-dimensional flamelets extracted from DNS solutions. The results show that while conventional 1D flamelet solutions can provide a good approximation of the jet flame structure, incorporating differential diffusion helps to accurately predict the flame front position. Furthermore, asymptotic scaling analysis and budget analysis of generalized flamelet equations are conducted for the extracted flamelets. It is found that multi-dimensional flamelet effects do have a substantial impact on the jet flame. Nevertheless, flame-normal diffusion is dominant over flame-tangential diffusion. These findings suggest that the 1D flamelet assumption is reasonable for the transcritical LOX/GH2 jet flame and that attention should be paid to incorporating differential diffusion effects in the modeling of transcritical LOX/GH2 jet flames.

跨临界燃烧的精确建模对高效火箭发动机的研制至关重要。一维火焰理论在跨临界和超临界燃烧模拟中得到了广泛的应用，但对多维火焰效应的综合分析仍然很少。为此，本文通过比较一维小火焰溶液和从DNS溶液中提取的多维小火焰溶液，对跨临界LOX/GH2射流火焰中的多维小火焰效应进行了先验分析。结果表明，虽然传统的一维火焰求解方法可以很好地逼近射流火焰结构，但加入微分扩散有助于准确预测火焰前缘位置。进一步，对提取的小波进行了广义小波方程的渐近尺度分析和预算分析。研究发现，多维火焰效应确实对射流火焰有很大的影响。然而，火焰法向扩散比火焰切向扩散占优势。这些结果表明，对于跨临界LOX/GH2射流火焰，1D小火焰假设是合理的，在跨临界LOX/GH2射流火焰的建模中应注意考虑差分扩散效应。

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引用次数: 0

Large eddy simulation of transient leading edge propagation in a turbulent lifted hydrogen jet flame 湍流提升型氢射流火焰前缘瞬态传播的大涡模拟

IF 5.2 2区工程技术 Q2 ENERGY & FUELS

Proceedings of the Combustion Institute

Pub Date : 2025-01-01 DOI: 10.1016/j.proci.2025.105827

Christoph D.K. Schumann , James C. Massey , Caleb J. Li , Nedunchezhian Swaminathan

A lifted turbulent jet flame involves partial premixing and exhibits a tribrachial flame structure at its leading edge (LE). Its propagation from the initial sparking location towards the final stabilisation height has rich physics. Large eddy simulation (LES) with flamelet-based reaction rate closure for partially premixed combustion is employed to study this propagation. The initial kernel grows radially in the rich region, and it is skewed by the oncoming flow as it is convected downstream. An LE is formed as the flame propagates radially into lean mixtures with low streamwise velocities. This LE encounters the lean limit, while a core flame continues to develop closer to the jet centreline, where the mixture reactivity and flow velocity are significantly large. Eventually, this core flame overtakes the LE in the lean mixture and upstream propagation ensues. The LE propagates mostly in the lean mixture, as the streamwise velocity in the vicinity of the jet core is high, although occasional rapid propagation is observed as the core flame encounters highly reactive mixture due to turbulence. Hence, the two flame branches are competing to form the LE. This behaviour is quite different to propagation in a lifted methane jet flame due to the increased reactivity and wider flammability limits of hydrogen. Turbulence plays a fundamental role during propagation for the formation of new upstream flame kernels, which evolve from pockets of hot reactants and fresh mixture. These kernels may be convected downstream causing the LE to recede. Eventually, the LE reaches a stationary state, and the flame root stabilises at a position where the burning mass flux is balanced by the flame normal advective mass flux. The LE does not encounter the value of the extinction dissipation rate for the mixture fraction during its evolution towards the stabilisation and at this location.

升力湍流射流火焰涉及部分预混，在前缘表现出三臂火焰结构。其从初始火花位置到最终稳定高度的传播具有丰富的物理性质。采用基于火焰的反应速率闭合大涡模拟（LES）对部分预混燃烧的这种传播进行了研究。初始核在富区呈放射状生长，并在向下游对流时被迎面而来的气流扭曲。当火焰沿径向传播成低流速的稀薄混合物时，就形成了LE。当核心火焰继续向靠近射流中心线的地方发展时，这种LE遇到了倾斜极限，在那里混合物的反应性和流动速度都非常大。最终，这个核心火焰在稀薄混合物中超过LE，然后上游传播。由于射流核心附近的流向速度高，LE主要在稀薄的混合物中传播，尽管当核心火焰遇到由于湍流引起的高度反应性混合物时，偶尔会观察到快速传播。因此，两个火焰分支正在竞争形成LE。由于氢气的反应性增加和可燃性限制，这种行为与在提升的甲烷喷射火焰中的传播完全不同。湍流在上游火焰核的形成过程中起着重要的作用，而上游火焰核是由热反应物和新鲜混合物形成的。这些核可能会向下游对流，导致LE后退。最终，LE达到稳态，火焰根部稳定在燃烧质量通量与火焰法向平流质量通量平衡的位置。在趋于稳定的过程中，在这个位置，LE不遇到混合分数的消光耗散率值。

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引用次数: 0

A theoretical study of 1-propanol H-abstractions and successive reactivity 1-丙醇h萃取及连续反应性的理论研究

IF 5.2 2区工程技术 Q2 ENERGY & FUELS

Proceedings of the Combustion Institute

Pub Date : 2025-01-01 DOI: 10.1016/j.proci.2025.105928

Sarah N. Elliott , Maristella Di Teodoro , Simone Vari , Luna Pratali Maffei , Zeynep Serinyel , Océane Clement , Claire Grégoire , Eric L. Petersen , Olivier Mathieu , Guillaume Dayma , Carlo Cavallotti

A mechanistic understanding of alcohol pyrolysis and oxidation is critical to their effective integration into the fuel industry. 1-propanol (1-C₃H₇OH) is a promising biofuel and, moreover, its mechanism is a foundation for that of larger alcohols. As part of a combined modeling-experimental-theoretical investigation into 1-C₃H₇OH, we explore the H abstractions from 1-C₃H₇OH with ab initio transition state theory-based master equation (AI-TST-ME) evaluations for the two abstractors, OH and H, that are influential during 1-C₃H₇OH combustion. We report branching fractions between the resulting C₃H₇O radicals (i.e., at 1500 K, for the OH abstractor: 0.40, 0.27, 0.24, and 0.09 to α-, β−, γ−, and ο−C₃H₇O; for the H abstractor: 0.80, 0.14, 0.06, and 0.00). The sensitivity to level of theory as well as the influence of multidimensional torsional effects are evaluated for the abstractions by OH. Notably, the correction for torsional coupling for the α−C₃H₇O is about half of that as for the β−C₃H₇O – fully neglecting the multidimensional effect, then, would lead to significantly different branching fractions. The subsequent dissociation of the C₃H₇O radicals to nine products, including CH₃, OH, ethene, ethyl radical, and H is also reported with AI-TST-ME computations. We find, however, that at relevant temperatures and pressures, very little 1-C₃H₇OH + OH collisionally stabilizes to thermalized C₃H₇O radicals (i.e., 7 % at 1 atm and 1500 K). Instead, the abundant, rovibrationally excited populations of C₃H₇O radicals promptly dissociate to the products. In the first exploration of the influence of non-thermal effects on the branching fractions to dissociation products, we find that H production enhances significantly (i.e., more than a factor of 2) at the cost of OH production.

了解酒精热解和氧化的机理对其有效整合到燃料工业至关重要。1-丙醇（1-C3H7OH）是一种很有前途的生物燃料，而且，它的机理为大醇的机理奠定了基础。作为1-C3H7OH的建模-实验-理论联合研究的一部分，我们利用基于过渡态理论的从头算主方程（AI-TST-ME）对影响1-C3H7OH燃烧过程的OH和H这两个抽象因子进行了评价，探讨了1-C3H7OH中H的抽象。我们报告了生成的C3H7O自由基之间的分支分数（即，在1500 K下，OH萃取剂：0.40,0.27,0.24和0.09到α-， β -， γ -和ο - C3H7O；对于H萃取剂：0.80,0.14,0.06和0.00）。评价了OH对理论层次的敏感性以及多维扭转效应对抽象的影响。值得注意的是，α - C3H7O的扭转耦合修正量约为β - C3H7O的一半，因此，完全忽略多维效应将导致明显不同的分支分数。随后的C3H7O自由基解离为九种产物，包括CH3， OH，乙烯，乙基自由基和H，也报道了ai - sts - me计算。然而，我们发现，在相应的温度和压力下，很少有1- c3h7oh + OH碰撞稳定为热化的C3H7O自由基（即在1atm和1500k时为7%）。相反，大量的、振动激发的C3H7O自由基迅速解离到产物上。在第一次探索非热效应对分支馏分对解离产物的影响时，我们发现以OH生产为代价，H的生产显著增加（即超过2倍）。

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引用次数: 0

Investigation of hot-spot-induced pre-ignition in methanol- and hydrogen-fueled spark-ignition engines 甲醇和氢燃料火花点火发动机的热点诱导预点火研究

IF 5.2 2区工程技术 Q2 ENERGY & FUELS

Proceedings of the Combustion Institute

Pub Date : 2025-01-01 DOI: 10.1016/j.proci.2025.105932

D. Golc , S. Esposito , M. Khosravi , J. Beeckmann , H. Pitsch

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