Constants of ignition delay model of diesel fuel surrogates with cetane numbers of 35 and 45, based on Cantera simulations

IF 1.8 4区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of The Brazilian Society of Mechanical Sciences and Engineering Pub Date : 2024-08-13 DOI:10.1007/s40430-024-05066-8
Paulo Gustavo Krejci Nunes, Waldyr Luiz Ribeiro Gallo
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Abstract

The study aims to present new constants of ignition delay based on the Arrhenius model for two diesel fuel surrogates formulated from four components (n-Hexadecane, Heptamethylnonane, Decahydro-naphthalene, and 1-Methyl-naphthalene) as a function of temperature and pressure, obtained by simulation in an adiabatic, homogeneous and constant pressure reactor using the Cantera simulator. The reaction was considered stoichiometric, with a temperature and pressure range varying from 700 to 2200 K and 40 to 120 atm, typical values found in the combustion chamber of turbocharged compression ignition engines. It was found that two-stage combustion occurs for temperatures between 700 and 1000 K (for pressure of 80 atm). When the combustion occurs in two-stages, we detail the ignition delay of each stage, and its first-stage fraction are presented. Surrogate fuels was modeled in 35 and 45 cetane numbers and 48 and 35 threshold soot index, respectively, to compare low and medium fuels in cetane numbers. The main application of these models relates to stochastic combustion models, which require fast models with low computational cost. The main differential of this study refers to its description of two-stage combustion, if it occurs. The model does not consider the physical ignition delay, referring to atomization, mixing and heating of the fuel. Results were compared with models from the literature, showing good agreement and presented intermediate values when compared with the literature.

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基于 Cantera 模拟的十六烷值为 35 和 45 的柴油代用燃料点火延迟模型常数
本研究旨在介绍基于阿伦尼乌斯模型的两种柴油代用燃料(由四种成分(正十六烷、七甲基壬烷、十氢萘和 1-甲基萘)配制而成)点火延迟的新常数,这些常数是利用 Cantera 模拟器在绝热、均质和恒压反应器中模拟得到的,是温度和压力的函数。反应被视为化学计量反应,温度和压力范围在 700 至 2200 K 和 40 至 120 atm 之间,这是涡轮增压压燃式发动机燃烧室中的典型值。研究发现,当温度在 700 至 1000 K 之间(压力为 80 atm)时,会发生两级燃烧。当燃烧发生在两个阶段时,我们详细说明了每个阶段的点火延迟及其第一阶段的分数。代用燃料的十六烷值分别为 35 和 45,阈值烟尘指数分别为 48 和 35,以比较中低十六烷值燃料。这些模型的主要应用与随机燃烧模型有关,随机燃烧模型需要计算成本低的快速模型。这项研究的主要差异在于它对两阶段燃烧(如果发生的话)的描述。该模型不考虑物理点火延迟,而是指燃料的雾化、混合和加热。研究结果与文献中的模型进行了比较,显示出良好的一致性,并提出了与文献比较的中间值。
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来源期刊
CiteScore
3.60
自引率
13.60%
发文量
536
审稿时长
4.8 months
期刊介绍: The Journal of the Brazilian Society of Mechanical Sciences and Engineering publishes manuscripts on research, development and design related to science and technology in Mechanical Engineering. It is an interdisciplinary journal with interfaces to other branches of Engineering, as well as with Physics and Applied Mathematics. The Journal accepts manuscripts in four different formats: Full Length Articles, Review Articles, Book Reviews and Letters to the Editor. Interfaces with other branches of engineering, along with physics, applied mathematics and more Presents manuscripts on research, development and design related to science and technology in mechanical engineering.
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