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A comparative study on the effects of NO2 addition on the auto-ignition behavior of n-heptane, iso-octane and toluene at engine relevant conditions
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-23 DOI: 10.1016/j.combustflame.2025.114118
Shijun Dong , Da Yao , A. Abd El-Sabor Mohamed , Jinhua Li , Wenxue Gao , Yang Cao , Zhaowen Wang , Jinhu Liang , Henry J. Curran , Xiaobei Cheng
It is necessary for gasoline surrogate models to simulate the effect of NOx addition on fuel auto-ignition behavior, as NOx can affect engine combustion via exhaust gas recirculation (EGR). Toluene is often used as a representative aromatic component in gasoline surrogate models, and hence it is important to investigate the effect of NOx addition on its auto-ignition behavior and to fully understand the interaction chemistry between toluene and NOx. In this paper, high-pressure shock tubes and a rapid compression machine are used to measure the ignition delay times (IDTs) of toluene in ‘air’ mixtures with and without the addition of nitrogen dioxide (NO2), at a pressure of 20 atm and at temperatures in the range 600–1400 K. The IDTs of n-heptane, iso-octane and a mixture of toluene/n-heptane/iso-octane are measured at the same conditions for comparison. The experimental results show that the auto-ignition behavior of toluene exhibits significantly different sensitivity to NO2 addition compared to n-heptane and iso-octane. NO2 significantly promotes the reactivity of toluene at low temperatures (600–1000 K), in which the IDTs decreased by two orders of magnitude when 1000 ppm of NO2 is added, whereas there is an order of magnitude decrease with the addition of 200 ppm NO2. The promoting effect of NO2 on toluene oxidation reduces significantly at temperatures above 1000 K. The experimental results also show that NO2 addition exhibits a slight promoting effect on the reactivity of n-heptane and iso-octane at temperatures above 750 K at the conditions studied. A kinetic model is proposed based on C3MechV3.3 in which the interaction chemistry between these gasoline surrogates and NOx is updated. The proposed kinetic model can simulate well the effect of NO2 addition on the auto-ignition behavior of these surrogates. Flux and sensitivity analyses are performed to highlight the important interaction reaction pathways.
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引用次数: 0
Two dimensional flame structure of oscillating burner-stabilized methane-air flames
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-23 DOI: 10.1016/j.combustflame.2025.114115
Ningyi Li , Viatcheslav Bykov , Anastasia Moroshkina , Evgeniy Sereshchenko , Vladimir Gubernov
The highly transient relaxational diffusive-thermal oscillations of flat burner-stabilized flames can be very attractive to probe the performance of detailed reaction mechanisms in the regimes close to ignition/extinction. In such regimes, certain reaction zones can travel over distances of the order of 10 mm and this raises an important question if one dimensional numerical models can be accurate in describing them. The question of quantitative comparison of modeling and experiments becomes crucial to study, to understand these regimes and to utilize them for validation. In this work, we experimentally investigate relaxational oscillations of methane-air flames on a flat porous burner with a surrounding nitrogen co-flow and perform fully resolved 2D numerical simulations of the same burner configuration, using a detailed reaction mechanism and molecular diffusion model, buoyancy and radiation, alongside corresponding experiments. The focus is on the effect of the nitrogen co-flow on the flame oscillations, which can only be studied numerically in 2D simulations due to the mutual effect of the complex flow field and flame dynamics. The results of both numerical and experimental approaches are found to be in quantitative agreement. They show that there is an optimal co-flow velocity that removes the secondary diffusion flame and extinguishes the edge flame settled in the stagnation flow region. This optimal regime makes the flame flatter and closer to a one-dimensional configuration and this is a most favorable condition for validation of kinetic mechanisms. The detailed data from the simulations will guide the design of the next generation of the burner configurations to study the kinetics and dynamics of complex fuels required for a sustainable energy transition.
Novelty and Significance Statement
The novelty of this research lies in the synergy of these modeling, computations with experimental measurements, allowing both parametric studies of the oscillation regime and deeper insights into the flame structure. These results are significant because they allow to develop more accurate burner configurations for studying flames near extinction and ignition conditions, which will be an important task for more complex fuels from renewable sources required for a sustainable energy transition. Ultimately, our understanding of the interplay between chemistry and diffusion controlled combustion regimes under transient conditions can be approved and validation data for e.g. chemical reaction mechanisms can be generated. The latter becomes extremely important since efficiency and pollutant mitigation issues require lean and chemistry controlled combustion processes used in the combustion facilities. Thus understanding, optimization and control of such regimes has become a crucial point for further development of the sustainable combustion.
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引用次数: 0
Analysis of combustion behavior and regression rate of hypergolic solid fuels in counterflow spray experiment
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-22 DOI: 10.1016/j.combustflame.2025.114132
Wei-Che Lin , Ray Peterson , Michael J. Bortner , Gregory Young
Recent studies have shown the advantages of hypergolic solid fuels in hybrid rockets, particularly their short ignition delays and simplified designs. However, research on their combustion behavior and regression rates remains limited. This study attempts to address some of these gaps using low-density polyethylene-based fuels embedded with sodium borohydride and 90 wt% hydrogen peroxide as the oxidizer. A modified counterflow spray experiment was employed, revealing unique combustion features and surface structures, such as char spots and bulges. A novel technique was developed to measure the fuel regression rate under an oxidizer spray, yielding averages between 0.39 to 0.52 mm/s at oxidizer mass flow rates of 0.38 to 0.43 g/s, significantly higher than those obtained with oxygen counterflow burners. Regression rates increased with higher flow rates and additive concentrations, primarily due to enhanced surface reactions. The measured combustion delay times were considerably longer than the ignition delay times observed in droplet tests, highlighting the importance of evaluating ignition performance under spray conditions. Reignition tests revealed longer ignition and combustion delay times compared to the first ignition, with averages increasing from 23 to 162 ms and 158 to 342 ms, respectively. Thermochemical analysis and Fourier transform infrared spectroscopy (FTIR) identified the char layer as primarily sodium metaborate tetrahydrate, which is identified as a cause for its reduced reactivity with the oxidizer during reignition.
最近的研究显示了混合火箭中使用双酚固体燃料的优势,特别是其较短的点火延迟和简化的设计。然而,对其燃烧行为和回归率的研究仍然有限。本研究尝试使用嵌入硼氢化钠和 90 wt%过氧化氢作为氧化剂的低密度聚乙烯基燃料来弥补其中的一些不足。研究采用了改良的逆流喷雾实验,揭示了独特的燃烧特征和表面结构,如焦斑和凸起。在氧化剂质量流量为 0.38 至 0.43 克/秒时,平均值为 0.39 至 0.52 毫米/秒,明显高于氧气逆流燃烧器的平均值。回归率随着流速和添加剂浓度的提高而增加,这主要是由于表面反应增强所致。测得的燃烧延迟时间大大长于液滴试验中观察到的点火延迟时间,这凸显了在喷雾条件下评估点火性能的重要性。复燃测试显示,与首次点火相比,点火和燃烧延迟时间更长,平均值分别从 23 毫秒增至 162 毫秒,从 158 毫秒增至 342 毫秒。热化学分析和傅立叶变换红外光谱(FTIR)确定炭层主要是偏硼酸钠四水合物,这也是其在复燃过程中与氧化剂反应性降低的原因。
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引用次数: 0
Modeling and validation: A comprehensive and robust surrogate kinetic model for oxidation of various biodiesels
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-22 DOI: 10.1016/j.combustflame.2025.114109
Lalit Y. Attarde, Krithika Narayanaswamy
In recent years, there has been a notable surge in experimental and kinetic modeling efforts concerning various biodiesels, their surrogates, and relevant molecules. This work culminates these research efforts to construct a comprehensive and robust surrogate kinetic model for various biodiesel fuels. This model has incorporated accurate chemistry and undergone extensive validation against a broad range of experimental data available for biodiesel. In order to accurately reproduce the combustion characteristics of biodiesel, methyl butanoate, methyl crotonate, 3-hexene, and n-dodecane are chosen as surrogate components. These molecules have been chosen to replicate the functional groups found in biodiesel methyl esters. Each surrogate component is firstly validated thoroughly against a wide array of experimental studies. The kinetics of each component are improved through careful rate assignments derived from various theoretical investigations. Subsequently, a surrogate mixture comprising these selected components is formulated by matching the functional groups of target fuels. This surrogate mechanism is used to validate the experimental data associated with various biodiesel fuels, their constituents, and methyl esters exhibiting similar functional groups to those present in actual biodiesel. The current kinetic model has demonstrated good agreement for various biodiesel fuels and their commonly used surrogates for a range of experimental studies, encompassing ignition delay times measured in shock tubes and rapid compression machines, laminar flame speeds, as well as species mole fractions measured in jet stirred reactors and laminar flow reactors.
Novelty and significance statement
This study introduces novel surrogate mixtures consisting of methyl butanoate, methyl crotonate, 3-hexene, and n-dodecane, formulated to predict the combustion characteristics of biodiesel. While several surrogate formulations for biodiesel exist in the literature, the novelty of this work lies in its extensive validation and reliable kinetic of the surrogate mixtures, which is leveraged from well-validated chemistry of each of these individual components. The study investigates whether selected small methyl esters and alkene can sufficiently capture combustion characteristics of molecules with similar functional groups. Currently, there are only two comprehensive biodiesel kinetic models in the literature, both developed over a decade ago, which have been widely used in subsequent studies for optimization and reduction. The new model presented in this study offers a more reliable chemistry while being relatively more compact, owing to its use of well validated small molecule surrogate components.
近年来,有关各种生物柴油、其替代物和相关分子的实验和动力学建模工作明显激增。这项工作将这些研究工作推向了高潮,为各种生物柴油燃料构建了一个全面而强大的代用动力学模型。该模型结合了精确的化学原理,并根据生物柴油的大量实验数据进行了广泛验证。为了准确再现生物柴油的燃烧特性,选择了丁酸甲酯、巴豆酸甲酯、3-己烯和正十二烷作为代用成分。选择这些分子是为了复制生物柴油甲酯中的官能团。首先根据大量实验研究对每种代用成分进行了全面验证。通过各种理论研究得出的仔细的速率分配,改进了每种成分的动力学。随后,通过匹配目标燃料的官能团,配制出由这些选定成分组成的代用混合物。这种代用机制被用来验证与各种生物柴油燃料、其成分以及与实际生物柴油中类似官能团的甲酯相关的实验数据。在一系列实验研究中,包括在冲击管和快速压缩机中测量的点火延迟时间、层流火焰速度,以及在喷射搅拌反应器和层流反应器中测量的物种摩尔分数,目前的动力学模型与各种生物柴油燃料及其常用的代用燃料具有良好的一致性。新颖性和重要性说明 本研究介绍了由丁酸甲酯、巴豆酸甲酯、3-己烯和正十二烷组成的新型替代混合物,用于预测生物柴油的燃烧特性。虽然文献中已有几种生物柴油的代用配方,但这项工作的新颖之处在于它对代用混合物进行了广泛的验证和可靠的动力学分析,而这些动力学分析是通过对这些单个成分的化学性质进行充分验证后得出的。该研究调查了所选的小甲酯和烯是否能充分捕捉具有类似官能团的分子的燃烧特性。目前,文献中只有两个全面的生物柴油动力学模型,这两个模型都是十多年前开发的,在随后的研究中被广泛用于优化和还原。本研究提出的新模型由于使用了经过充分验证的小分子替代成分,因此化学性质更加可靠,同时相对更加紧凑。
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引用次数: 0
Combustion characteristics and primary particle size of soot in ethylene/propylene-air coflow flames under dynamic pressure rise environment
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-21 DOI: 10.1016/j.combustflame.2025.114113
Jingru Zheng , Xiaolei Zhang , Suk Ho Chung , Longhua Hu
The effect of dynamic pressure rise rate on the burning characteristics and soot particle size in laminar coflow flames of ethylene and propylene is studied. Flame characteristics are observed at constant fuel flow rates under five pressure rise rates. Soot particles are collected using a thermophoretic sampling method at a pressure of 65 kPa during the pressure increase, and the primary soot particle diameters in ethylene flames are measured using a transmission electron microscope (TEM). The results show that the flame height increases with chamber pressure until 65 kPa, then slightly decreases. The flame becomes shorter with a higher pressure rise rate, influenced by both diffusion and buoyancy effects. As pressure increases, the transverse diffusion of fuel molecules diminishes, causing the flame to become slender. Simultaneously, the buoyancy effect enhances air entrainment, contributing to a reduction in flame height. A relationship between the flame height, pressure and dynamic pressure rise rate is derived based on the Burke-Schumann theory by assuming the pressure as a function of time. The proposed model can successfully predict the experimental data. The length of the soot-free main reaction zone (exhibiting a blue color) decreases with increasing pressure and is longer at smaller pressure rise rates. The relationship between the blue flame zone length and the dynamic pressure rise rate, which is characterized by soot formation time, correlates well with experimental results. The measured soot particle sizes range from 25 to 35 nm. The soot particle sizes are larger at lower pressure rise rates. The fractal dimension decreases with increasing pressure rise rates, while the pre-factor increases as the pressure rise rates become higher.
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引用次数: 0
A fundamental investigation of the pyrolysis chemistry of Oxymethylene Ethers. Part I: Quantum chemical calculations and kinetic model development
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-21 DOI: 10.1016/j.combustflame.2025.114121
Kevin De Ras , Olivier Herbinet , Frédérique Battin-Leclerc , Yann Fenard , Luc-Sy Tran , Guillaume Vanhove , Joris W. Thybaut , Kevin M. Van Geem
Oxymethylene ethers (OMEs) have emerged as a promising and sustainable alternative for fossil-based fuels in recent years. This class of synthetic fuels can be produced from captured CO2 with renewable electricity, so-called e-fuels, using carbon capture and utilization technology resulting in environmentally cleaner combustion. However, before OMEs can be used globally, it is essential to have a thorough understanding of their radical decomposition chemistry. In this study, combined experimental and kinetic modeling work is conducted to unravel the pyrolysis chemistry of oxymethylene ether-3 (OME-3), oxymethylene ether-4 (OME-4), and oxymethylene ether-5 (OME-5). A detailed kinetic model for pyrolysis of these long-chain OMEs with elementary reaction steps is developed based on first principles with the automatic kinetic model generation tool ‘Genesys’. The unimolecular decomposition pathways are explored by constructing potential energy surfaces, which highlight the importance of formaldehyde elimination reactions. In addition, rate rules are regressed for the unimolecular decomposition reactions of radicals, based on the quantum chemical results, to enable extrapolation of the kinetic data. The developed kinetic model is validated using experimental datasets from the literature, and benchmarking against other pyrolysis models demonstrates better predictive performance. The experimental observations are accurately predicted, on average within the uncertainty margin (∼10 mol% relative) for major compounds, without fitting model parameters. Part II of this study presents six newly acquired experimental datasets from jet-stirred and tubular reactors, additional kinetic model validation, and a comprehensive model analysis through rate of production and sensitivity analyses.
{"title":"A fundamental investigation of the pyrolysis chemistry of Oxymethylene Ethers. Part I: Quantum chemical calculations and kinetic model development","authors":"Kevin De Ras ,&nbsp;Olivier Herbinet ,&nbsp;Frédérique Battin-Leclerc ,&nbsp;Yann Fenard ,&nbsp;Luc-Sy Tran ,&nbsp;Guillaume Vanhove ,&nbsp;Joris W. Thybaut ,&nbsp;Kevin M. Van Geem","doi":"10.1016/j.combustflame.2025.114121","DOIUrl":"10.1016/j.combustflame.2025.114121","url":null,"abstract":"<div><div>Oxymethylene ethers (OMEs) have emerged as a promising and sustainable alternative for fossil-based fuels in recent years. This class of synthetic fuels can be produced from captured CO<sub>2</sub> with renewable electricity, so-called e-fuels, using carbon capture and utilization technology resulting in environmentally cleaner combustion. However, before OMEs can be used globally, it is essential to have a thorough understanding of their radical decomposition chemistry. In this study, combined experimental and kinetic modeling work is conducted to unravel the pyrolysis chemistry of oxymethylene ether-3 (OME-3), oxymethylene ether-4 (OME-4), and oxymethylene ether-5 (OME-5). A detailed kinetic model for pyrolysis of these long-chain OMEs with elementary reaction steps is developed based on first principles with the automatic kinetic model generation tool ‘Genesys’. The unimolecular decomposition pathways are explored by constructing potential energy surfaces, which highlight the importance of formaldehyde elimination reactions. In addition, rate rules are regressed for the unimolecular decomposition reactions of radicals, based on the quantum chemical results, to enable extrapolation of the kinetic data. The developed kinetic model is validated using experimental datasets from the literature, and benchmarking against other pyrolysis models demonstrates better predictive performance. The experimental observations are accurately predicted, on average within the uncertainty margin (∼10 mol% relative) for major compounds, without fitting model parameters. Part II of this study presents six newly acquired experimental datasets from jet-stirred and tubular reactors, additional kinetic model validation, and a comprehensive model analysis through rate of production and sensitivity analyses.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"275 ","pages":"Article 114121"},"PeriodicalIF":5.8,"publicationDate":"2025-03-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143682848","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Multi-phase hypergolic ignition model
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-21 DOI: 10.1016/j.combustflame.2025.114114
David A. Castaneda , Joseph K. Lefkowitz , Benveniste Natan
A novel approach for modeling hypergolic ignition is presented, validated, and used to successfully predict ignition delay times for a hybrid rocket propellant configuration. This configuration employs a hypergolic additive (sodium borohydride) that allows two non-hypergolic reactants (polyethylene and hydrogen peroxide) to gain hypergolic capabilities. The model considers multiple phases and multiple species, heterogeneous and homogeneous chemical reactions, mass transfer between phases, and heat transfer. The transient behavior of the various chemical and thermal properties involved in hypergolic ignition is studied. In addition, a parametric investigation is conducted to predict ignition delay times as functions of multiple variables such as additive loading, oxidizer concentration, and initial propellant temperatures, among others. The results are presented in the form of ignition delay time contour maps. The heat release rate is shown to be controlled mostly by hypergolic chemical reactions. Gas homogeneous reactions only take place during the last portion of the ignition process and are the ones responsible for ultimately leading to a gas thermal runaway. The proper inclusion of the vaporization and pyrolysis of the propellants is found to be crucial since these determine the formation of a gas phase, where ignition is achieved. It is found that the vaporization of the liquid oxidizer is the controlling mass transfer mechanism for the hybrid rocket configuration considered. The model successfully predicts the minimum hypergolic additive loading and the range of oxidizer-to-fuel ratios required for ignition. It is found that the optimal oxidizer-to-fuel ratio leading to the shortest ignition delay time is mostly a function of additive loading. In addition, it is found that pressure, propellant initial temperature, and oxidizer concentration, have a major influence on ignition delay times and that they barely affect the optimal oxidizer-to-fuel ratio. The presented model, although evaluated for the hybrid rocket configuration, is considered to be applicable for any hypergolic propellant configuration.
本文介绍了一种新的双醇点火建模方法,对其进行了验证,并用于成功预测混合火箭推进剂配置的点火延迟时间。这种配置采用了一种高热效应添加剂(硼氢化钠),使两种非高热效应反应物(聚乙烯和过氧化氢)获得高热效应能力。该模型考虑了多相和多物种、异相和均相化学反应、相间传质和传热。研究了双酚点火所涉及的各种化学和热特性的瞬态行为。此外,还进行了参数调查,以预测点火延迟时间与添加剂装载量、氧化剂浓度和推进剂初始温度等多个变量的函数关系。研究结果以点火延迟时间等值线图的形式呈现。结果表明,热释放率主要受高热化学反应控制。气体均相反应只发生在点火过程的最后阶段,是最终导致气体热失控的原因。研究发现,适当加入推进剂的汽化和热解反应至关重要,因为这些反应决定了气相的形成,并在气相中实现点火。研究发现,液体氧化剂的汽化是所考虑的混合火箭构型的控制传质机制。模型成功地预测了点火所需的最小双酚添加剂装载量和氧化剂与燃料的比例范围。研究发现,导致最短点火延迟时间的最佳氧化剂燃料比主要是添加剂装载量的函数。此外,研究还发现,压力、推进剂初始温度和氧化剂浓度对点火延迟时间有很大影响,但它们几乎不会影响最佳氧化剂与燃料比率。所提出的模型虽然是针对混合火箭配置进行评估的,但被认为适用于任何双质推进剂配置。
{"title":"Multi-phase hypergolic ignition model","authors":"David A. Castaneda ,&nbsp;Joseph K. Lefkowitz ,&nbsp;Benveniste Natan","doi":"10.1016/j.combustflame.2025.114114","DOIUrl":"10.1016/j.combustflame.2025.114114","url":null,"abstract":"<div><div>A novel approach for modeling hypergolic ignition is presented, validated, and used to successfully predict ignition delay times for a hybrid rocket propellant configuration. This configuration employs a hypergolic additive (sodium borohydride) that allows two non-hypergolic reactants (polyethylene and hydrogen peroxide) to gain hypergolic capabilities. The model considers multiple phases and multiple species, heterogeneous and homogeneous chemical reactions, mass transfer between phases, and heat transfer. The transient behavior of the various chemical and thermal properties involved in hypergolic ignition is studied. In addition, a parametric investigation is conducted to predict ignition delay times as functions of multiple variables such as additive loading, oxidizer concentration, and initial propellant temperatures, among others. The results are presented in the form of ignition delay time contour maps. The heat release rate is shown to be controlled mostly by hypergolic chemical reactions. Gas homogeneous reactions only take place during the last portion of the ignition process and are the ones responsible for ultimately leading to a gas thermal runaway. The proper inclusion of the vaporization and pyrolysis of the propellants is found to be crucial since these determine the formation of a gas phase, where ignition is achieved. It is found that the vaporization of the liquid oxidizer is the controlling mass transfer mechanism for the hybrid rocket configuration considered. The model successfully predicts the minimum hypergolic additive loading and the range of oxidizer-to-fuel ratios required for ignition. It is found that the optimal oxidizer-to-fuel ratio leading to the shortest ignition delay time is mostly a function of additive loading. In addition, it is found that pressure, propellant initial temperature, and oxidizer concentration, have a major influence on ignition delay times and that they barely affect the optimal oxidizer-to-fuel ratio. The presented model, although evaluated for the hybrid rocket configuration, is considered to be applicable for any hypergolic propellant configuration.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"276 ","pages":"Article 114114"},"PeriodicalIF":5.8,"publicationDate":"2025-03-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143684400","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Experimental exploration of the N-containing soot precursors in C2H4-NH3 co-flow diffusion flames
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-20 DOI: 10.1016/j.combustflame.2025.114104
Fei Ren, Zhuohang Li, Yezeng Fan, Jinze Li, Zhenyingnan Zhang, Ang Li, Zhan Gao, Lei Zhu, Zhen Huang
The chemical effect of ammonia can reduce the formation of soot precursors in hydrocarbon fuel flames. The nitrogen from ammonia can combine with hydrocarbon species to reduce polycyclic aromatic hydrocarbons (PAHs) while forming nitrogen-containing polycyclic aromatic hydrocarbons (NPAH). In this work, an in-depth experimental investigation was conducted to identify the chemical effect of ammonia on the changes of N-containing functional groups in soot surface and the NPAH formation in C2H4-NH3 co-flow diffusion flames. The X-ray photoelectron spectroscopy (XPS) and microscopic imaging infrared spectrometer (MIR) analysis were carried out to investigate the chemical composition of soot particles and determine the types and structural characteristics of functional groups on the soot surface. The results showed that ammonia addition increased the proportion of nitrogen and oxygen in soot and enriched the nitrogen/oxygen-containing functional groups on the soot surface. The soot sampled in ethylene flames with and without ammonia addition has similar chemical composition and surface functional groups. In particular, the aromatic CN group was found in the soot from ethylene-ammonia diffusion flames. Also, the NPAH containing CN bond was further determined through gas chromatography-mass spectrometry (GC-MS) analysis. The observed NPAH are mainly cyano substituted-PAHs such as 1-Naphthalenecarbonitrile (A2CN, m/z=153), 5-acenaphthylenecarbonitrile (A2R5CN, m/z=177), etc. It indicated that the active sites on the aromatic surface facilitated the binding of HCN and CN bond to generate the cyano substituted-PAHs such as A2CN and A2R5CN. But the inhibitory effect of NPAH containing CN bond on the formation of large PAHs and soot is limited. This experimental study confirmed that ammonia promoted the formation of NPAH containing CN bond in soot.
氨的化学效应可减少碳氢化合物燃料火焰中烟尘前体的形成。氨中的氮可与碳氢化合物结合,减少多环芳烃(PAHs),同时形成含氮多环芳烃(NPAH)。本研究通过深入实验研究了氨对 C2H4-NH3 共流扩散火焰中烟尘表面含氮官能团变化和 NPAH 形成的化学影响。通过 X 射线光电子能谱(XPS)和显微成像红外光谱仪(MIR)分析,研究了烟尘颗粒的化学组成,确定了烟尘表面官能团的类型和结构特征。结果表明,氨的加入增加了烟尘中氮和氧的比例,丰富了烟尘表面的含氮/氧官能团。在乙烯火焰中取样的烟尘中,添加氨和不添加氨的烟尘具有相似的化学成分和表面官能团。特别是在乙烯-氨扩散火焰的烟尘中发现了芳香族 CN 基团。此外,还通过气相色谱-质谱(GC-MS)分析进一步确定了含有 CN 键的 NPAH。观察到的 NPAH 主要是氰基取代的 PAHs,如 1-萘甲腈(A2CN,m/z=153)、5-苊烯甲腈(A2R5CN,m/z=177)等。这表明芳香表面的活性位点促进了 HCN 和 CN 键的结合,生成了 A2CN 和 A2R5CN 等氰基取代的 PAHs。但含有 CN 键的 NPAH 对大型 PAHs 和烟尘形成的抑制作用有限。本实验研究证实,氨促进了烟尘中含有 CN 键的 NPAH 的形成。
{"title":"Experimental exploration of the N-containing soot precursors in C2H4-NH3 co-flow diffusion flames","authors":"Fei Ren,&nbsp;Zhuohang Li,&nbsp;Yezeng Fan,&nbsp;Jinze Li,&nbsp;Zhenyingnan Zhang,&nbsp;Ang Li,&nbsp;Zhan Gao,&nbsp;Lei Zhu,&nbsp;Zhen Huang","doi":"10.1016/j.combustflame.2025.114104","DOIUrl":"10.1016/j.combustflame.2025.114104","url":null,"abstract":"<div><div>The chemical effect of ammonia can reduce the formation of soot precursors in hydrocarbon fuel flames. The nitrogen from ammonia can combine with hydrocarbon species to reduce polycyclic aromatic hydrocarbons (PAHs) while forming nitrogen-containing polycyclic aromatic hydrocarbons (NPAH). In this work, an in-depth experimental investigation was conducted to identify the chemical effect of ammonia on the changes of N-containing functional groups in soot surface and the NPAH formation in C<sub>2</sub>H<sub>4</sub>-NH<sub>3</sub> co-flow diffusion flames. The X-ray photoelectron spectroscopy (XPS) and microscopic imaging infrared spectrometer (MIR) analysis were carried out to investigate the chemical composition of soot particles and determine the types and structural characteristics of functional groups on the soot surface. The results showed that ammonia addition increased the proportion of nitrogen and oxygen in soot and enriched the nitrogen/oxygen-containing functional groups on the soot surface. The soot sampled in ethylene flames with and without ammonia addition has similar chemical composition and surface functional groups. In particular, the aromatic C<img>N group was found in the soot from ethylene-ammonia diffusion flames. Also, the NPAH containing C<img>N bond was further determined through gas chromatography-mass spectrometry (GC-MS) analysis. The observed NPAH are mainly cyano substituted-PAHs such as 1-Naphthalenecarbonitrile (A2CN, m/z=153), 5-acenaphthylenecarbonitrile (A2R5CN, m/z=177), etc. It indicated that the active sites on the aromatic surface facilitated the binding of HCN and C<img>N bond to generate the cyano substituted-PAHs such as A2CN and A2R5CN. But the inhibitory effect of NPAH containing C<img>N bond on the formation of large PAHs and soot is limited. This experimental study confirmed that ammonia promoted the formation of NPAH containing C<img>N bond in soot.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"276 ","pages":"Article 114104"},"PeriodicalIF":5.8,"publicationDate":"2025-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143684397","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
DDT run-up distance for stoichiometric hydrogen-methane-oxygen measured in an orifice plate filled tube
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-20 DOI: 10.1016/j.combustflame.2025.114124
Chuanyu Pan , Xishi Wang , Gaby Ciccarelli
Flame acceleration and deflagration-to-detonation transition (DDT) was studied in a 2.88-m, 7.6-cm inner-diameter transparent round tube filled with repeating 50 % blockage-ratio orifice plates. Stoichiometric hydrogen/methane/oxygen, with different hydrogen-to-methane mole ratios, and argon-diluted stoichiometric hydrogen-oxygen mixtures were tested. These mixtures span a range of detonation cell structure regularity. The reactivity of the mixture was controlled by varying the initial pressure, from the DDT critical pressure to a maximum of 40 kPa. Flame velocity was measured from high-speed video. The DDT run-up distance was obtained directly from the video images, and soot foils were used to confirm the DDT location at the critical initial pressure and to measure the detonation cell size at the end of the tube void of obstacles. The DDT run-up distance was shorter for methane containing mixtures at the lowest initial pressure near the DDT limit but was the same for all mixtures at pressures greater than 15 kPa. For each mixture, the DDT run-up distance decreased with the detonation cell size according to an inverse power-law. For a given detonation cell size, the DDT run-up distance decreases with increased methane-fraction. Therefore, for a given orifice diameter, at the DDT limit (where the orifice diameter roughly equals the detonation cell size), the DDT run-up distance for methane-containing mixtures is shorter than for 100 % hydrogen. This, and the fact that a higher initial pressure is required for methane containing mixtures to have the same cell size, needs to be considered when assessing the explosion hazard of hydrogen/methane mixtures.
{"title":"DDT run-up distance for stoichiometric hydrogen-methane-oxygen measured in an orifice plate filled tube","authors":"Chuanyu Pan ,&nbsp;Xishi Wang ,&nbsp;Gaby Ciccarelli","doi":"10.1016/j.combustflame.2025.114124","DOIUrl":"10.1016/j.combustflame.2025.114124","url":null,"abstract":"<div><div>Flame acceleration and deflagration-to-detonation transition (DDT) was studied in a 2.88-m, 7.6-cm inner-diameter transparent round tube filled with repeating 50 % blockage-ratio orifice plates. Stoichiometric hydrogen/methane/oxygen, with different hydrogen-to-methane mole ratios, and argon-diluted stoichiometric hydrogen-oxygen mixtures were tested. These mixtures span a range of detonation cell structure regularity. The reactivity of the mixture was controlled by varying the initial pressure, from the DDT critical pressure to a maximum of 40 kPa. Flame velocity was measured from high-speed video. The DDT run-up distance was obtained directly from the video images, and soot foils were used to confirm the DDT location at the critical initial pressure and to measure the detonation cell size at the end of the tube void of obstacles. The DDT run-up distance was shorter for methane containing mixtures at the lowest initial pressure near the DDT limit but was the same for all mixtures at pressures greater than 15 kPa. For each mixture, the DDT run-up distance decreased with the detonation cell size according to an inverse power-law. For a given detonation cell size, the DDT run-up distance decreases with increased methane-fraction. Therefore, for a given orifice diameter, at the DDT limit (where the orifice diameter roughly equals the detonation cell size), the DDT run-up distance for methane-containing mixtures is shorter than for 100 % hydrogen. This, and the fact that a higher initial pressure is required for methane containing mixtures to have the same cell size, needs to be considered when assessing the explosion hazard of hydrogen/methane mixtures.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"276 ","pages":"Article 114124"},"PeriodicalIF":5.8,"publicationDate":"2025-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143684418","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Effect of hydroxypropyl methylcellulose and ferric chloride on hypergolic ignition of solidified ethanol fuels
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-03-20 DOI: 10.1016/j.combustflame.2025.114126
Jerin John , Purushothaman Nandagopalan , Ankur Miglani , Pranay Mudaliar , Seung Wook Baek
This study investigates the hypergolic ignition of reaction-driven solidified ethanol (RDSE) fuels, focusing on the effects of varying concentrations of hydroxypropyl methylcellulose (HPMC) gellant and ferric chloride (FeCl3) dopant. Fourier Transform Infrared Spectroscopy (FTIR) and thermogravimetric analysis (TGA) are employed to examine molecular interactions and thermal properties. FTIR results indicate that no new covalent bonds are formed upon adding FeCl3, whereas interactions primarily governed by weak hydrogen and ionic bonds. The apparent activation energy (Ea) has been determined for the fuel samples using iso-conversional model-free kinetics approach and found that Ea decreased with HPMC and FeCl3 concentrations. Hypergolic ignition delay tests were attempted with the droplet study rocket grade hydrogen peroxide (90 % RGHP; H2O2) as an oxidizer, demonstrated that increasing HPMC concentration by 3 wt.% reduced ignition delay by ∼20 %, while a 5 wt.% increase in FeCl3 concentration led to a ∼25 % reduction. Higher fuel temperatures enhanced the wetting and spreading behavior of H2O2 droplets, improving oxidizer-fuel interaction and reducing ignition delay. Overall, solidification of ethanol using HPMC with FeCl3 eliminates the catalyst as FeCl3 acts as both catalyst and binding agent.
{"title":"Effect of hydroxypropyl methylcellulose and ferric chloride on hypergolic ignition of solidified ethanol fuels","authors":"Jerin John ,&nbsp;Purushothaman Nandagopalan ,&nbsp;Ankur Miglani ,&nbsp;Pranay Mudaliar ,&nbsp;Seung Wook Baek","doi":"10.1016/j.combustflame.2025.114126","DOIUrl":"10.1016/j.combustflame.2025.114126","url":null,"abstract":"<div><div>This study investigates the hypergolic ignition of reaction-driven solidified ethanol (RDSE) fuels, focusing on the effects of varying concentrations of hydroxypropyl methylcellulose (HPMC) gellant and ferric chloride (FeCl<sub>3</sub>) dopant. Fourier Transform Infrared Spectroscopy (FTIR) and thermogravimetric analysis (TGA) are employed to examine molecular interactions and thermal properties. FTIR results indicate that no new covalent bonds are formed upon adding FeCl<sub>3</sub>, whereas interactions primarily governed by weak hydrogen and ionic bonds. The apparent activation energy (<span><math><msub><mi>E</mi><mi>a</mi></msub></math></span>) has been determined for the fuel samples using iso-conversional model-free kinetics approach and found that <span><math><msub><mi>E</mi><mi>a</mi></msub></math></span> decreased with HPMC and FeCl<sub>3</sub> concentrations. Hypergolic ignition delay tests were attempted with the droplet study rocket grade hydrogen peroxide (90 % RGHP; H<sub>2</sub>O<sub>2</sub>) as an oxidizer, demonstrated that increasing HPMC concentration by 3 wt.% reduced ignition delay by ∼20 %, while a 5 wt.% increase in FeCl<sub>3</sub> concentration led to a ∼25 % reduction. Higher fuel temperatures enhanced the wetting and spreading behavior of H<sub>2</sub>O<sub>2</sub> droplets, improving oxidizer-fuel interaction and reducing ignition delay. Overall, solidification of ethanol using HPMC with FeCl<sub>3</sub> eliminates the catalyst as FeCl<sub>3</sub> acts as both catalyst and binding agent.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"276 ","pages":"Article 114126"},"PeriodicalIF":5.8,"publicationDate":"2025-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143684417","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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Combustion and Flame
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