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Dynamic behaviors of burning droplet suspended on NiCr-wire with applied AC electric field
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-05 DOI: 10.1016/j.combustflame.2025.114024
Seung Hyun Kim , Jeong Park , Suk Ho Chung , Chun Sang Yoo
Effect of applied AC electric field on burning n-decane droplet suspended on NiCr wire (0.5 mm in diameter) was investigated experimentally by varying the AC frequency fAC (10−1000 Hz) and voltage VAC (1−5 kV). Three initial diameters of n-decane droplets were tested. Due to the difference in droplet surface temperature between the edge region and the central bottom region of the suspended droplet, caused by the heat transfer through the wire from the flame, an internal circulation is generated inside the droplet during burning, which enhances the evaporation rate, subsequently increases the flame width and height. When an AC is applied, the dynamic behaviors of droplet and flame are significantly influenced. Depending on VAC and fAC, six regimes can be classified: dripping (DP) of droplet (Regime I) for large droplets due to decreased surface tension from heat transfer through the wire; vertical oscillation (OS) of the droplet due to a vertical dielectrophoretic force (II); lateral spread (LS) and OS of droplet (III) caused by a horizontal dielectrophoretic force between wire sections with and without the droplet; LS and a flame-spitting (FS) phenomenon due to excessive LS (IV); LS and formation of flame vortex (FV) near flame edges due to induced magnetic field (V); and the simultaneous occurrence of LS, FS, and FV (VI). The behavior of vertical oscillation was examined from the solution of the linearly-perturbed Rayleigh-Plesset equation, where the OS amplitude of the droplet increases with VAC and decreases with fAC. The mechanism of lateral spread was investigated by analyzing the onset conditions, specifically in terms of VAC and fAC. For burning droplets, it was observed that the vertical oscillatory motion is enhanced due to the imbalance in surface tension between the upper and lower surfaces of the droplet and the internal flow becomes faster due to the reduced droplet viscosity. The internal flow response time decreases with fAC, leading to an increase in oscillation amplitude with increasing VAC and/or fAC. The mechanism of the induced magnetic field was tested through the onset conditions having a constant critical magnetic field intensity. The normalized droplet lifetime is characterized by their related physical parameters, including the gradient of radial electric field intensity at the central surface of droplet, fAC, droplet diameter, and flame width and height. The droplet lifetime shows a strong correlation with the combination of these parameters in both the OS and LS cases.
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引用次数: 0
An adaptive implicit time-integration scheme for stiff chemistry based on Jacobian tabulation method
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-05 DOI: 10.1016/j.combustflame.2025.113997
Sihang Rao , Wenyuan Zhou , Wang Han , Yihao Tang , Xu Xu
The use of detailed chemical mechanisms in modeling chemically reacting flows often results in large computational costs. In this study, a stiff ODE solver, combining the backward differentiation formula (BDF) with a novel Jacobian tabulation (JT) method, was developed to significantly reduce the computational cost of solving chemical ordinary differential equations (ODEs) with detailed chemistry. The resulting BDF-JT method offers several key advantages: (a) it accelerates the evaluation and factorization of the Jacobian matrix during the BDF solution process through a two-level dynamic tabulation; (b) a properly selected set of state parameters governs the identification of similar Jacobians and their factorizations within the tabulation system; and (c) efficient look-up and dynamic updates of the tabulation are enabled using hash tables. The accuracy and efficiency of the BDF-JT method were systematically compared against the original BDF and CVODE solvers across a range of scenarios, including homogeneous auto-ignition, laminar flame propagation, and oblique detonation waves (ODW). The results showed that the proposed method had negligible effects on accuracy under the studied tolerances. In terms of computational efficiency, the BDF-JT method achieved significant speedup, reducing the computational cost of solving chemical ODEs by a factor of 173.7 in the auto-ignition case with a 2885-species mechanism and by a factor of 41.3 for ODW combustion with a 1384-species mechanism, with higher efficiency observed for more complex reaction systems. Overall, the BDF-JT method demonstrates strong potential for drastically reducing computational costs while maintaining high accuracy in large-scale combustion simulations, making it a valuable tool for high-fidelity combustion simulation.
Novelty and Significance Statement
There is an urgent need to incorporate more realistic chemical mechanisms in modeling chemical reacting flows. Due to the large computational cost of using detailed chemical kinetics, operator-splitting schemes along with several stiff ODE solvers have been studied and demonstrated performance. Unfortunately, most stiff ODE solvers are likely developed trading off accuracy for performance. The present study provides a dynamic tabulation method for chemical Jacobian in the implicit ODE solvers. As such, it helps to accelerate the computations in combustion simulations without sacrificing accuracy.
在化学反应流建模中使用详细的化学机制往往会导致计算成本过高。在本研究中,开发了一种结合了后向微分公式(BDF)和新型雅各布表法(JT)的刚性 ODE 求解器,以显著降低求解具有详细化学机制的化学常微分方程(ODE)的计算成本。由此产生的 BDF-JT 方法具有几个关键优势:(a) 在 BDF 求解过程中,它通过两级动态制表加速了雅各矩阵的评估和因式分解;(b) 适当选择的一组状态参数可在制表系统中识别相似的雅各及其因式分解;(c) 利用哈希表实现了制表的高效查找和动态更新。在各种情况下,包括均质自燃、层流火焰传播和斜向爆轰波(ODW),系统地比较了 BDF-JT 方法与原始 BDF 和 CVODE 求解器的精度和效率。结果表明,在所研究的公差范围内,拟议方法对精度的影响可以忽略不计。在计算效率方面,BDF-JT 方法取得了显著的加速效果,在采用 2885 种机理的自燃情况下,化学 ODE 的求解计算成本降低了 173.7 倍,在采用 1384 种机理的 ODW 燃烧情况下,降低了 41.3 倍,而且在更复杂的反应系统中观察到了更高的效率。总之,BDF-JT 方法在大规模燃烧模拟中保持高精度的同时,在大幅降低计算成本方面展现出强大的潜力,使其成为高保真燃烧模拟的重要工具。由于使用详细的化学动力学计算成本较高,人们研究了算子拆分方案和几种刚性 ODE 求解器,并证明了它们的性能。遗憾的是,大多数刚性 ODE 求解器在开发过程中可能会牺牲精度和性能。本研究为隐式 ODE 求解器中的化学雅各布提供了一种动态制表方法。因此,它有助于在不牺牲精度的情况下加快燃烧模拟的计算速度。
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引用次数: 0
Computational diagnostics and characterization of combustion recession in diesel sprays
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-05 DOI: 10.1016/j.combustflame.2025.113993
F.J. Arguelles , M.D. Fagade , J. Mehra , C. Xu , N. Sekularac , X.H. Fang
<div><div>While low-temperature combustion (LTC) strategies have been found to mitigate nitrogen oxides and particulate matter emissions in diesel engines, studies have also associated LTC with an increase in unburnt hydrocarbons. With more recent studies on diesel after end-of-injection (AEOI), combustion recession is identified as a phenomenon where at near nozzle region, high-temperature ignition (HTI) combustion can propagate back to the nozzle tip consuming the unburnt hydrocarbons AEOI. Current literature has suggested that combustion recession is controlled by auto-ignition. However, high-fidelity simulations and detailed analysis of such a mechanism are missing. In this study, comprehensive Large Eddy Simulations of a reacting spray at “Spray A” conditions are performed, where detailed analysis of combustion recession concerning flame morphology and propagation modes are included. In particular, this study demonstrated for the first time that while combustion recession is mainly auto-ignition dominated (consistent with the literature), a cool flame was found to deflagrate towards the richer regions of the mixture, promoting mixing and increasing the mixture temperature. This leads to HTI kernels, which then grow and develop as deflagrative waves, therefore sustaining the combustion recession process. The study also detailed the extinction mechanism of combustion: the entrainment wave will overlean the near-nozzle mixtures, rendering it unable to support HTI, which leads to the extinction of the upstream flame AEOI in lower reactivity mixtures. Combustion recession is also observed to be contingent on the chemical and diffusion processes, even at low scalar dissipation rates. Finally, a new criterion for combustion recession based on chemical explosive mode is proposed and validated with previous combustion recession index to quantify the extent of HTI in near-nozzle mixtures AEOI. The newly developed metric combined with a previous experimentally-based metric can provide simple but valuable measurements of the degree and propensity of the upstream flame AEOI.</div><div><strong>Novelty and Significance Statement</strong></div><div>This work covers the literature gap in detailing the spray after end-of-injection combustion recession mechanisms. The study is significant, suggesting that while combustion recession is auto-ignition-dominated, deflagration modes were found, for the first time, to exist within the kernels via a cool flame at the end of injection. With further analysis, the deflagration modes were found to promote mixing at the end of injection which is deemed critical in sustaining combustion recession. The extinction mechanisms on the other hand were associated with the significant role of entrainment waves after end-of-injection. To generalize the findings of our study, a novel combustion recession metric based on the chemical explosive mode is proposed where agreement is found with the experimental observations. The new metri
研究发现,低温燃烧(LTC)策略可减少柴油发动机中的氮氧化物和颗粒物排放,但研究也发现低温燃烧与未燃烧碳氢化合物的增加有关。最近对柴油机喷射末端(AEOI)的研究发现,燃烧衰退是指在喷嘴附近区域,高温点火(HTI)燃烧可传播回喷嘴顶端,消耗未燃碳氢化合物的 AEOI 现象。现有文献认为,燃烧后退是由自燃控制的。然而,目前还缺乏对这种机制的高保真模拟和详细分析。本研究对 "喷雾 A "条件下的反应喷雾进行了全面的大涡流模拟,其中包括有关火焰形态和传播模式的燃烧衰退详细分析。特别是,该研究首次证明,虽然燃烧衰退主要以自燃为主(与文献一致),但发现冷火焰会向混合物的富集区爆燃,促进混合并提高混合物温度。这导致 HTI 核,然后作为爆燃波增长和发展,从而维持燃烧衰退过程。研究还详细阐述了燃烧的熄灭机制:夹带波会使喷嘴附近的混合物过剩,使其无法支持 HTI,从而导致低反应性混合物中的上游火焰 AEOI 熄灭。即使在低标量耗散率的情况下,燃烧衰退也取决于化学和扩散过程。最后,提出了一种基于化学爆炸模式的燃烧衰退新标准,并与之前的燃烧衰退指数进行了验证,以量化近喷嘴混合物 AEOI 中 HTI 的程度。新开发的指标与之前基于实验的指标相结合,可对上游火焰 AEOI 的程度和倾向进行简单而有价值的测量。这项研究意义重大,它表明虽然燃烧衰退以自燃为主,但首次发现在喷射结束时通过冷却火焰在内核中存在爆燃模式。通过进一步分析,发现爆燃模式促进了喷射末端的混合,这被认为是维持燃烧衰退的关键。另一方面,熄灭机制与喷射结束后的夹带波的重要作用有关。为了推广我们的研究结果,我们提出了一种基于化学爆炸模式的新型燃烧衰退指标,结果与实验观测结果一致。新指标可为三维数值模拟提供有效的计算诊断工具,在识别燃烧衰退倾向和程度方面与之前的实验指标相辅相成。
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引用次数: 0
Theoretical investigation on unimolecular decomposition network of n-propylamine with advanced kinetic methods
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-05 DOI: 10.1016/j.combustflame.2025.113996
Zhenpeng Zhang , Chong Li , Yanlei Shang , Haiyong Zhao , Sheng-Nian Luo
<div><div>Unimolecular decomposition network of <span><math><mi>n</mi></math></span>-propylamine (NPA) is theoretically investigated. Twenty intramolecular H-shift/H<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span> elimination reactions and three bond dissociation reactions are identified, including some new reactions producing singlet species. Among these reactions, only one intramolecular H-shift reaction that yields C<span><math><msub><mrow></mrow><mrow><mn>3</mn></mrow></msub></math></span>H<span><math><msub><mrow></mrow><mrow><mn>6</mn></mrow></msub></math></span> + NH<span><math><msub><mrow></mrow><mrow><mn>3</mn></mrow></msub></math></span> and three bond dissociation reactions are dominant. The M06-2X/jun-cc-pVTZ and M06-L/jun-cc-pVTZ methods are adopted for kinetic calculations given their well-balanced accuracy and computational costs. The reaction-path variational transition state theory and variable reaction coordinate variational transition state theory are applied to determine the high-pressure limit rate constants of the intramolecular H-shift reaction and bond dissociation reactions, respectively, and the multi-structure torsional anharmonicity and small-curvature tunneling correction are considered. The pressure-dependent rate constants are also determined using the system-specific quantum Rice–Ramsperger–Kassel theory at 700–2000 K and 0.001–100 atm. The C<span><math><msub><mrow></mrow><mrow><mi>α</mi></mrow></msub></math></span>–C<span><math><msub><mrow></mrow><mrow><mi>β</mi></mrow></msub></math></span> bond dissociation reaction that produces CH<span><math><msub><mrow></mrow><mrow><mn>3</mn></mrow></msub></math></span>CH<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span> and CH<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span>NH<span><math><msub><mrow></mrow><mrow><mn>2</mn></mrow></msub></math></span> radicals is the most important with a branching ratio larger than 0.85 over the investigated temperature range. Our calculated rate constants agree well with the literature data and effectively capture the effect of pressure on the rate constants within the uncertainty in energy determination. With our calculations, a literature combustion model is updated and performs better in predicting the speciation data during the NPA pyrolysis and ignition delay times of NPA.</div><div><strong>Novelty and Significance statement</strong></div><div>This work theoretically investigates the unimolecular decomposition network of <span><math><mi>n</mi></math></span>-propylamine (NPA) by using the advanced reaction-path variational transition state theory and the variable reaction coordinate variational transition state theory for reactions with tight and loose transition states, respectively, with the consideration of multi-structure torsional anharmonicity and small-curvature tunneling correction. Some novel unimolecular decomposition reactions producing singlet specie
{"title":"Theoretical investigation on unimolecular decomposition network of n-propylamine with advanced kinetic methods","authors":"Zhenpeng Zhang ,&nbsp;Chong Li ,&nbsp;Yanlei Shang ,&nbsp;Haiyong Zhao ,&nbsp;Sheng-Nian Luo","doi":"10.1016/j.combustflame.2025.113996","DOIUrl":"10.1016/j.combustflame.2025.113996","url":null,"abstract":"&lt;div&gt;&lt;div&gt;Unimolecular decomposition network of &lt;span&gt;&lt;math&gt;&lt;mi&gt;n&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt;-propylamine (NPA) is theoretically investigated. Twenty intramolecular H-shift/H&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; elimination reactions and three bond dissociation reactions are identified, including some new reactions producing singlet species. Among these reactions, only one intramolecular H-shift reaction that yields C&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;H&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;6&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; + NH&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; and three bond dissociation reactions are dominant. The M06-2X/jun-cc-pVTZ and M06-L/jun-cc-pVTZ methods are adopted for kinetic calculations given their well-balanced accuracy and computational costs. The reaction-path variational transition state theory and variable reaction coordinate variational transition state theory are applied to determine the high-pressure limit rate constants of the intramolecular H-shift reaction and bond dissociation reactions, respectively, and the multi-structure torsional anharmonicity and small-curvature tunneling correction are considered. The pressure-dependent rate constants are also determined using the system-specific quantum Rice–Ramsperger–Kassel theory at 700–2000 K and 0.001–100 atm. The C&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;α&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;–C&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;β&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; bond dissociation reaction that produces CH&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;3&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;CH&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; and CH&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt;NH&lt;span&gt;&lt;math&gt;&lt;msub&gt;&lt;mrow&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/math&gt;&lt;/span&gt; radicals is the most important with a branching ratio larger than 0.85 over the investigated temperature range. Our calculated rate constants agree well with the literature data and effectively capture the effect of pressure on the rate constants within the uncertainty in energy determination. With our calculations, a literature combustion model is updated and performs better in predicting the speciation data during the NPA pyrolysis and ignition delay times of NPA.&lt;/div&gt;&lt;div&gt;&lt;strong&gt;Novelty and Significance statement&lt;/strong&gt;&lt;/div&gt;&lt;div&gt;This work theoretically investigates the unimolecular decomposition network of &lt;span&gt;&lt;math&gt;&lt;mi&gt;n&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt;-propylamine (NPA) by using the advanced reaction-path variational transition state theory and the variable reaction coordinate variational transition state theory for reactions with tight and loose transition states, respectively, with the consideration of multi-structure torsional anharmonicity and small-curvature tunneling correction. Some novel unimolecular decomposition reactions producing singlet specie","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"274 ","pages":"Article 113996"},"PeriodicalIF":5.8,"publicationDate":"2025-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143193337","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
Quantitative studies of instabilities of confined spherically expanding flames: Application to flame propagation and autoignition of natural gas blends with hydrogen at engine-relevant conditions
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-02 DOI: 10.1016/j.combustflame.2025.114009
Kyuho Van , Anguo Hu , Jung Z. Fang , Tushar K. Bera , Allen A. Aradi , Sandeep K. Jain , Fokion N. Egolfopoulos
The availability of accurate fundamental combustion properties at engine-relevant conditions is of paramount importance in testing kinetic and transport models so that they can be used in large-scale simulations of practical devices. However, a literature search reveals that flame data can be scarce at engine-relevant conditions, and those that are available may be of limited value due to large uncertainties associated with experiments at high temperatures and pressures that can render the flames unstable. The main contribution of this study was the introduction of one-dimensional and multi-dimensional direct numerical simulations to quantify the onset of flame instabilities at conditions used in measuring laminar flame speeds. This is a deviation from the traditional approaches that use theoretical predictions and/or circumstantial evidence to vet and interpret experimental data. To that end, the confined spherically expanding flame method was used to measure laminar flame speeds for reacting mixtures of hydrogen-natural gas blends, for pressures ranging from 8 to 30 atm, and for unburned mixture temperatures ranging from 420 to 530 K. This approach proved to be successful as the predicted and experimental results were consistent with each other, and the reported data herein were measured for conditions that the direct numerical simulations revealed that they resulted in stable flames throughout all stages of propagation. As expected, the laminar flame speed increases with hydrogen addition, and this increase was found to be slightly more notable compared to recently published data under similar conditions for hydrogen-methane flames. Additionally, under suitably chosen conditions, autoignition in the end gas was induced during the compression stage of stable flame propagation, and ignition delay times with remarkably low repeatability scatter were measured through the rapid changes in the pressure-time derivatives. The autoignition studies included n-pentane as an additive to achieve autoignition within the available times in the existing constant-volume spherical facility. For blends of hydrogen with natural gas and n-pentane, a two-stage ignition behavior was observed, and the hydrogen addition resulted in the reduction of ignition delay times. All reported data were modeled, offering insights into the mechanisms governing flame propagation and autoignition. The results of the present study are expected to contribute to ongoing endeavors related to hydrogen utilization and decarbonization in the transportation sector.
在发动机相关条件下,获得准确的基本燃烧特性对于测试动力学和传输模型至关重要,这样这些模型才能用于实际设备的大规模模拟。然而,文献检索显示,在发动机相关条件下的火焰数据可能非常稀少,而且由于在高温高压下进行的实验具有很大的不确定性,可能会导致火焰不稳定,因此现有的火焰数据价值有限。本研究的主要贡献在于引入了一维和多维直接数值模拟,以量化在测量层流火焰速度条件下火焰不稳定性的发生。这有别于使用理论预测和/或间接证据来审核和解释实验数据的传统方法。为此,我们采用了封闭球形膨胀火焰法来测量氢气-天然气混合物反应混合物的层焰速度,压力范围为 8 至 30 atm,未燃烧混合物温度范围为 420 至 530 K。事实证明,这种方法是成功的,因为预测结果和实验结果是一致的,本文所报告的数据是在直接数值模拟显示会导致火焰在所有传播阶段都保持稳定的条件下测量的。正如预期的那样,层流火焰的速度会随着氢气的加入而增加,而且与最近公布的氢气-甲烷火焰在类似条件下的数据相比,这种增加更为显著。此外,在适当选择的条件下,在火焰稳定传播的压缩阶段诱发了末端气体的自燃,并通过压力-时间导数的快速变化测得了重复性散差极低的点火延迟时间。自燃研究将正戊烷作为添加剂,以便在现有恒容球形设备的可用时间内实现自燃。对于氢气与天然气和正戊烷的混合物,观察到了两阶段点火行为,氢气的添加导致了点火延迟时间的缩短。所有报告的数据都经过建模处理,有助于深入了解火焰传播和自燃的机理。预计本研究的结果将有助于正在进行的与氢气利用和交通领域脱碳有关的工作。
{"title":"Quantitative studies of instabilities of confined spherically expanding flames: Application to flame propagation and autoignition of natural gas blends with hydrogen at engine-relevant conditions","authors":"Kyuho Van ,&nbsp;Anguo Hu ,&nbsp;Jung Z. Fang ,&nbsp;Tushar K. Bera ,&nbsp;Allen A. Aradi ,&nbsp;Sandeep K. Jain ,&nbsp;Fokion N. Egolfopoulos","doi":"10.1016/j.combustflame.2025.114009","DOIUrl":"10.1016/j.combustflame.2025.114009","url":null,"abstract":"<div><div>The availability of accurate fundamental combustion properties at engine-relevant conditions is of paramount importance in testing kinetic and transport models so that they can be used in large-scale simulations of practical devices. However, a literature search reveals that flame data can be scarce at engine-relevant conditions, and those that are available may be of limited value due to large uncertainties associated with experiments at high temperatures and pressures that can render the flames unstable. The main contribution of this study was the introduction of one-dimensional and multi-dimensional direct numerical simulations to quantify the onset of flame instabilities at conditions used in measuring laminar flame speeds. This is a deviation from the traditional approaches that use theoretical predictions and/or circumstantial evidence to vet and interpret experimental data. To that end, the confined spherically expanding flame method was used to measure laminar flame speeds for reacting mixtures of hydrogen-natural gas blends, for pressures ranging from 8 to 30 atm, and for unburned mixture temperatures ranging from 420 to 530 K. This approach proved to be successful as the predicted and experimental results were consistent with each other, and the reported data herein were measured for conditions that the direct numerical simulations revealed that they resulted in stable flames throughout all stages of propagation. As expected, the laminar flame speed increases with hydrogen addition, and this increase was found to be slightly more notable compared to recently published data under similar conditions for hydrogen-methane flames. Additionally, under suitably chosen conditions, autoignition in the end gas was induced during the compression stage of stable flame propagation, and ignition delay times with remarkably low repeatability scatter were measured through the rapid changes in the pressure-time derivatives. The autoignition studies included <em>n</em>-pentane as an additive to achieve autoignition within the available times in the existing constant-volume spherical facility. For blends of hydrogen with natural gas and <em>n</em>-pentane, a two-stage ignition behavior was observed, and the hydrogen addition resulted in the reduction of ignition delay times. All reported data were modeled, offering insights into the mechanisms governing flame propagation and autoignition. The results of the present study are expected to contribute to ongoing endeavors related to hydrogen utilization and decarbonization in the transportation sector.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"274 ","pages":"Article 114009"},"PeriodicalIF":5.8,"publicationDate":"2025-02-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143193352","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
Simplified radiation and soot models for buoyant diffusion flames: Quantitative investigation of fuel mixing effects
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-01 DOI: 10.1016/j.combustflame.2024.113904
Wenbin Yao, Haidong Liu, Zehua Yang, Xiao Chen, Shouxiang Lu
Simplified radiation and soot models were proposed to provide a simple yet effective method predicting flame radiation and soot characteristics for buoyant diffusion flames. To explore the quantitative effects of fuel mixing and validate the proposed models, LII measurement of soot distribution and multi-point measurement of radiation flux were conducted for different fuel mixtures and different mixing ratios. Characteristic length scales, including the height of soot inception, the height of maximum soot volume fraction and the height of soot oxidation in the soot distributions, were determined by the fuel type and mixing ratio, and resulted in different maximum soot volume fractions. The axial distribution of soot volume fraction, maximum soot volume fraction, soot volume and soot yield can be predicted by the simplified soot model based on the critical mixture fractions. The probability density function of axial soot volume fraction can be described by an exponential function related to the non-sooty probability and maximum soot volume fraction. In addition, flame radiation power presents a linear correlation with soot volume, and flame radiation fraction of buoyant diffusion flame of fuel mixtures presents a linear relationship with the maximum soot volume fraction, which is in agreement with the simplified radiation model proposed in this work.
{"title":"Simplified radiation and soot models for buoyant diffusion flames: Quantitative investigation of fuel mixing effects","authors":"Wenbin Yao,&nbsp;Haidong Liu,&nbsp;Zehua Yang,&nbsp;Xiao Chen,&nbsp;Shouxiang Lu","doi":"10.1016/j.combustflame.2024.113904","DOIUrl":"10.1016/j.combustflame.2024.113904","url":null,"abstract":"<div><div>Simplified radiation and soot models were proposed to provide a simple yet effective method predicting flame radiation and soot characteristics for buoyant diffusion flames. To explore the quantitative effects of fuel mixing and validate the proposed models, LII measurement of soot distribution and multi-point measurement of radiation flux were conducted for different fuel mixtures and different mixing ratios. Characteristic length scales, including the height of soot inception, the height of maximum soot volume fraction and the height of soot oxidation in the soot distributions, were determined by the fuel type and mixing ratio, and resulted in different maximum soot volume fractions. The axial distribution of soot volume fraction, maximum soot volume fraction, soot volume and soot yield can be predicted by the simplified soot model based on the critical mixture fractions. The probability density function of axial soot volume fraction can be described by an exponential function related to the non-sooty probability and maximum soot volume fraction. In addition, flame radiation power presents a linear correlation with soot volume, and flame radiation fraction of buoyant diffusion flame of fuel mixtures presents a linear relationship with the maximum soot volume fraction, which is in agreement with the simplified radiation model proposed in this work.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"272 ","pages":"Article 113904"},"PeriodicalIF":5.8,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143102433","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
An experimental and modeling study on indene oxidation: Emphasizing the competing kinetics between PAH oxidative decomposition and mass growth
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-01 DOI: 10.1016/j.combustflame.2024.113912
Yuwen Deng , Zaili Xiong , Jijun Guo , Chen Huang , Long Zhao , Meirong Zeng , Zhongyue Zhou , Wenhao Yuan , Fei Qi
Fundamental knowledge about the production and oxidation chemistry of polycyclic aromatic hydrocarbons (PAHs) is essential for developing predictive soot models. In contrast to the significant progress in understanding the formation/growth kinetics of PAHs, the detailed oxidation kinetics of PAHs remains to be fully established. This study investigates the oxidation kinetics of indene, the simplest PAH, as a foundational step for examining larger PAHs. Experiments were conducted in a flow reactor at temperatures from 850 to 1350 K, under a pressure of 0.04 atm and an equivalence ratio of 0.5. Characteristic products were quantified using synchrotron vacuum ultraviolet photoionization mass spectrometry, including large resonance-stabilized PAH radicals with 3–4 aromatic rings. Results indicate that even under highly oxidative conditions, the mass growth pathways of indene remain competitive, leading to the production of various large PAHs. This phenomenon is unique to indene oxidation and has not been observed in other bicyclic aromatics. A detailed kinetic model was developed to interpret these findings, revealing that PAH formation is predominantly driven by the indenyl radical. This study further calculates the rate coefficients for the dominant mass growth pathway of indenyl, specifically its self-recombination reaction, to enhance predictions of indenyl and bi-indene. Notably, while spiran and bridging mechanisms are comparably important in cyclopentadienyl mass growth, the spiran mechanism is favored for indenyl, suggesting that the addition of a benzenoid ring significantly alters the reactivity of cyclopenta-like radicals. Comparative analysis with indene pyrolysis experiments reveals that under oxidative conditions, the indenyl radical preferentially decomposes into smaller species, e.g., cyclopentadienyl or cyclopentadiene, thereby enhancing the yields of PAHs that depend on C5 species as precursors. In the early reaction stage (<1220 K), oxidation reactions promote indenyl formation, thus increasing the proportion of mass growth products. However, at higher temperatures (>1220 K), enhanced oxidation reactions of indenyl lead to its decomposition, outcompeting mass growth reactions and sharply reducing the proportion of mass growth products.
{"title":"An experimental and modeling study on indene oxidation: Emphasizing the competing kinetics between PAH oxidative decomposition and mass growth","authors":"Yuwen Deng ,&nbsp;Zaili Xiong ,&nbsp;Jijun Guo ,&nbsp;Chen Huang ,&nbsp;Long Zhao ,&nbsp;Meirong Zeng ,&nbsp;Zhongyue Zhou ,&nbsp;Wenhao Yuan ,&nbsp;Fei Qi","doi":"10.1016/j.combustflame.2024.113912","DOIUrl":"10.1016/j.combustflame.2024.113912","url":null,"abstract":"<div><div>Fundamental knowledge about the production and oxidation chemistry of polycyclic aromatic hydrocarbons (PAHs) is essential for developing predictive soot models. In contrast to the significant progress in understanding the formation/growth kinetics of PAHs, the detailed oxidation kinetics of PAHs remains to be fully established. This study investigates the oxidation kinetics of indene, the simplest PAH, as a foundational step for examining larger PAHs. Experiments were conducted in a flow reactor at temperatures from 850 to 1350 K, under a pressure of 0.04 atm and an equivalence ratio of 0.5. Characteristic products were quantified using synchrotron vacuum ultraviolet photoionization mass spectrometry, including large resonance-stabilized PAH radicals with 3–4 aromatic rings. Results indicate that even under highly oxidative conditions, the mass growth pathways of indene remain competitive, leading to the production of various large PAHs. This phenomenon is unique to indene oxidation and has not been observed in other bicyclic aromatics. A detailed kinetic model was developed to interpret these findings, revealing that PAH formation is predominantly driven by the indenyl radical. This study further calculates the rate coefficients for the dominant mass growth pathway of indenyl, specifically its self-recombination reaction, to enhance predictions of indenyl and bi-indene. Notably, while spiran and bridging mechanisms are comparably important in cyclopentadienyl mass growth, the spiran mechanism is favored for indenyl, suggesting that the addition of a benzenoid ring significantly alters the reactivity of cyclopenta-like radicals. Comparative analysis with indene pyrolysis experiments reveals that under oxidative conditions, the indenyl radical preferentially decomposes into smaller species, e.g., cyclopentadienyl or cyclopentadiene, thereby enhancing the yields of PAHs that depend on C<sub>5</sub> species as precursors. In the early reaction stage (&lt;1220 K), oxidation reactions promote indenyl formation, thus increasing the proportion of mass growth products. However, at higher temperatures (&gt;1220 K), enhanced oxidation reactions of indenyl lead to its decomposition, outcompeting mass growth reactions and sharply reducing the proportion of mass growth products.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"272 ","pages":"Article 113912"},"PeriodicalIF":5.8,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143102618","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
Role of hydrogen enrichment in ammonia forced ignition at elevated pressures
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-01 DOI: 10.1016/j.combustflame.2024.113908
Lei Wang, Xingqian Mao, Jinguang Li, Haiqiao Wei, Gequn Shu, Jiaying Pan
Numerous studies have demonstrated that hydrogen enrichment can improve ammonia reactivity, leading to enhanced ignition and combustion performance. However, the role of hydrogen enrichment in forced ignition of ammonia, especially at elevated pressures, remains not fully understood. This study employed a localized energy deposition technique to initiate the forced ignition of ammonia/hydrogen mixtures. The role of hydrogen ratio and ignition energy in ignition and flame kernel initiation was numerically investigated, and the critical ignition conditions were identified by assessing the correlations between heat release and thermal diffusion. The results show that the forced ignition at low pressures involves four traditional stages, whereas only two stages are present at high pressures, i.e., ignition assisted flame kernel propagation and normal laminar flame propagation. The weakening stretching responses at high pressures cause the flame kernel to propagate outward without additional ignition energy. Then deposited ignition energy mainly heats ignition kernels and increases the local temperature, thereby reducing ignition delay time and accelerating ignition initiation. Hydrogen enrichment enhancing ignition performance is mainly due to the changed fuel property and reduced ignition delay time. Kinetic analysis suggests that this enhancement is primarily attributed to the increased sensitivity of H+O2=O+OH and the substantial H generation from the reverse of NH3+H=NH2+H2, both of which promote the chain branching of H+O2=O+OH. Besides, successful ignition also depends on the competition between chemical heat release and thermal diffusion. Chemical heat release dominates within a timescale of ∼0.1 ms, while thermal diffusion prevails beyond the threshold. Hydrogen enrichment can significantly reduce minimum ignition energy, but this tendency becomes less pronounced when hydrogen ratio exceeds 20 %.
{"title":"Role of hydrogen enrichment in ammonia forced ignition at elevated pressures","authors":"Lei Wang,&nbsp;Xingqian Mao,&nbsp;Jinguang Li,&nbsp;Haiqiao Wei,&nbsp;Gequn Shu,&nbsp;Jiaying Pan","doi":"10.1016/j.combustflame.2024.113908","DOIUrl":"10.1016/j.combustflame.2024.113908","url":null,"abstract":"<div><div>Numerous studies have demonstrated that hydrogen enrichment can improve ammonia reactivity, leading to enhanced ignition and combustion performance. However, the role of hydrogen enrichment in forced ignition of ammonia, especially at elevated pressures, remains not fully understood. This study employed a localized energy deposition technique to initiate the forced ignition of ammonia/hydrogen mixtures. The role of hydrogen ratio and ignition energy in ignition and flame kernel initiation was numerically investigated, and the critical ignition conditions were identified by assessing the correlations between heat release and thermal diffusion. The results show that the forced ignition at low pressures involves four traditional stages, whereas only two stages are present at high pressures, i.e., ignition assisted flame kernel propagation and normal laminar flame propagation. The weakening stretching responses at high pressures cause the flame kernel to propagate outward without additional ignition energy. Then deposited ignition energy mainly heats ignition kernels and increases the local temperature, thereby reducing ignition delay time and accelerating ignition initiation. Hydrogen enrichment enhancing ignition performance is mainly due to the changed fuel property and reduced ignition delay time. Kinetic analysis suggests that this enhancement is primarily attributed to the increased sensitivity of H+O<sub>2</sub>=O+OH and the substantial H generation from the reverse of NH<sub>3</sub>+H=NH<sub>2</sub>+H<sub>2</sub>, both of which promote the chain branching of H+O<sub>2</sub>=O+OH. Besides, successful ignition also depends on the competition between chemical heat release and thermal diffusion. Chemical heat release dominates within a timescale of ∼0.1 ms, while thermal diffusion prevails beyond the threshold. Hydrogen enrichment can significantly reduce minimum ignition energy, but this tendency becomes less pronounced when hydrogen ratio exceeds 20 %.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"272 ","pages":"Article 113908"},"PeriodicalIF":5.8,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143102619","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
Publication / Copyright Information
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-01 DOI: 10.1016/S0010-2180(24)00645-X
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引用次数: 0
Tabulated chemistry approach for detonation simulations
IF 5.8 2区 工程技术 Q2 ENERGY & FUELS Pub Date : 2025-02-01 DOI: 10.1016/j.combustflame.2024.113878
Alexandra Baumgart, Matthew X. Yao, Guillaume Blanquart
Chemistry modeling in detonations typically relies on two broad approaches: simplified models with one- or two-step chemistry, and detailed chemistry. These approaches require choosing between computational efficiency or physical accuracy. To reduce the cost of chemistry while maintaining accurate physics, tabulated chemistry has been used extensively for flames/deflagrations in the low Mach number framework. In the simplest tabulated chemistry model for premixed flames, a progress variable, describing the progress of reactions in the system, is transported in the simulation. This progress variable is then used to look up all other species, transport properties, and thermodynamic variables from a pre-computed table. The present work extends the tabulated chemistry method to detonations. Even in non-reacting compressible flow simulations, the enthalpy and specific heat capacity are required; to describe these thermodynamic variables, the temperature is selected as a second table coordinate. The two table coordinates are able to capture virtually all variations in the progress variable source term. The Zel’dovich–von Neumann–Döring (ZND) model is found to be the most appropriate one-dimensional problem for generation of the table. The ZND tabulation approach is validated for both one-dimensional stable and pulsating and two-dimensional regular and irregular detonations in various H2-O2 mixtures. The tabulated chemistry simulations are able to reproduce the detailed chemistry results in terms of propagation speed, cellular structures, and source term statistics. For hydrogen detonations, the computational cost of scalar transport is reduced by a factor of 9 and the cost of the chemistry is reduced by a factor of 17. More substantial computational savings are expected for hydrocarbon fuels.
Novelty and significance statement
Detonations are often challenging to simulate due to the significant cost of integrating accurate chemical models. In deflagrations, this cost has been reduced by pre-computing the chemistry and collecting the information into a lookup table to be used at runtime. Although chemistry tabulation has been adapted recently for supersonic combustion, such as in scramjets, the typical assumptions of these approaches do not apply to detonations. We propose a new tabulated chemistry approach, valid for detonations and reproducing critical parameters such as induction zone length and detonation velocity. The key novelty lies in (1) the use of progress variable and temperature as the coordinates for tabulation, and (2) the selection of one-dimensional Zel’dovich–von Neumann–Döring detonations as the relevant physical problem to be tabulated. The new model significantly reduces the cost of simulations.
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引用次数: 0
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Combustion and Flame
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