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A chemical mechanism for low to high temperature oxidation of methylcyclohexane as a component of transportation fuel surrogates

机译:用作运输燃料替代物的甲基环己烷的低温至高温氧化的化学机理

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Surrogate fuels consisting of a mixture of well-studied hydrocarbons are often used to model real fuels in typical combustion studies. A major challenge, however, is the capability to design compact and reliable kinetic models that capture all the specificities of the simpler, but still multi-component surrogates. This task is further complicated by the diverse nature of the hydrocarbons commonly considered as potential surrogate components, since they typically result in large detailed reaction schemes. Towards addressing this challenge, the present work proposes a single, compact, and reliable chemical mechanism, that can accurately describe the oxidation of a wide range of fuels, which are important components of surrogate fuels. A well-characterized mechanism appropriate for the oxidation of smaller hydrocarbon species (Blanquart et al., 2009), as well as several substituted aromatic species and n-dodecane (Narayanaswamy et al., 2010, 2014), well suited as a base to model surrogates, has now been extended to describe the oxidation of methylcyclohexane, a representative of the cyclic alkane class, which is often used in jet fuel surrogates. To ensure compactness of the kinetic scheme, a short mechanism for the low to high temperature oxidation of methylcyclohexane is extracted from the detailed scheme of Fitz et al. (2007) and integrated in a systematic way into the previous model. Rate coefficient changes based on recent recommendations from literature, and an additional concerted elimination pathway important at moderate to low temperatures are introduced to the resulting chemical mechanism, which improve the model predictions. Extensive validation of the revised kinetic model is performed using a wide range of experimental conditions and data sets. Published by Elsevier Inc. on behalf of The Combustion Institute.
机译:由典型碳氢化合物混合物组成的替代燃料通常用于典型燃烧研究中的真实燃料建模。然而,主要的挑战是设计紧凑而可靠的动力学模型的能力,以捕获更简单但仍是多组分替代物的所有特异性。通常被认为是潜在的替代组分的碳氢化合物的多样性使该任务更加复杂,因为它们通常会导致大量详细的反应方案。为了解决这一挑战,本工作提出了一种单一,紧凑且可靠的化学机制,该机制可准确描述多种燃料的氧化,而这些燃料是替代燃料的重要组成部分。具有良好特征的机制适合氧化较小的烃类(Blanquart等,2009)以及几种取代的芳香族和正十二烷(Narayanaswamy等,2010,2014),非常适合作为替代模型的替代品,现在已扩展到描述甲基环己烷的氧化反应,这是环烷烃类的代表,常用于航空燃料替代品。为确保动力学方案的紧凑性,从Fitz等人的详细方案中提取了甲基环己烷从低温到高温氧化的简短机理。 (2007年),并以系统的方式集成到以前的模型中。根据文献的最新建议,速率系数发生了变化,并且在中至低温条件下重要的附加协同消除途径被引入了所得的化学机理,从而改善了模型预测。使用广泛的实验条件和数据集对修订后的动力学模型进行了广泛的验证。由Elsevier Inc.代表燃烧研究所出版。

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