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A new jet fuel surrogate formulated by emulating the distribution of pyrolysis products obtained from shock tube experiments

机译:通过模拟从冲击管实验中获得的热解产品的分布来配制的新型喷射燃料替代品

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摘要

A new jet fuel surrogate is developed by emulating the distribution of pyrolysis products obtained from shock tube experiments. The distribution of pyrolysis products is described by the use of a series of pyrolysis curves, which refers to a graphical depiction of the concentrations of pyrolysis products plotted against temperatures. Besides, the matching on chemical properties of jet fuel, including molecular weight (MW), hydrogen/oxygen ratio (H/C ratio), derived cetane number (DCN), lower heating value (LHV) and threshold sooting index (TSI), is also taken into account during the formulation process. The new surrogate is a mixture of n-decane, iso-cetane and m-xylene, and these three components are selected through the simulation of pyrolytic process based on the consideration that their mixture can provide similar pyrolysis curves to the target fuel. The validity of the new surrogate has been evaluated extensively against available experimental results from homogeneous reaction systems and low dimensional premixed flames. Meanwhile, a definition of "Error function" is introduced to quantitatively analyze the agreement between calculated values by surrogate and measured data of Jet A. As a reference, the predictive capabilities of four surrogates published in the last ten years and one hybrid-chemistry model for jet fuel are also investigated under the same conditions. According to the simulated results, the new surrogate with a detailed chemical mechanism from CRECK Modeling group (Version 1412) is capable of presenting reasonable predictions on the major combustion behaviors of Jet A across a wide range of conditions, such as ignition delay time, laminar burning velocity and oxidative products distribution.
机译:通过模拟从冲击管实验中获得的热解产品的分布来开发新的喷射燃料代理。通过使用一系列热解曲线描述热解产物的分布,这是指绘制温度的热解产物浓度的图形描述。此外,射流燃料的化学性质的匹配,包括分子量(MW),氢气/氧比(H / C比),衍生的十六烷数(DCN),较低的加热值(LHV)和阈值烟灰指数(TSI),在制定过程中也被考虑在内。新的替代物是N-癸烷,异甲烷和M-二甲苯的混合物,并且通过基于考虑它们的混合物可以为目标燃料提供类似的热解曲线来模拟热解过程来选择这三种组分。新代理的有效性已被广泛评估均匀反应系统和低维预混火焰的可用实验结果。同时,引入了“误差函数”的定义,以定量分析由射架A的代理和测量数据之间计算值之间的协议。作为参考,在过去十年和一个混合化学模型中发表的四种替代品的预测能力对于在相同条件下还研究了喷射燃料。根据模拟结果,具有来自克鲁克建模组(版本1412)的详细化学机制的新代理能够呈现对喷射A跨越各种条件的主要燃烧行为的合理预测,例如点火延迟时间,层燃烧的速度和氧化产品分布。

著录项

  • 来源
    《Fuel》 |2021年第1期|118874.1-118874.9|共9页
  • 作者单位

    Tsinghua Univ Ctr Combust Energy Beijing 10084 Peoples R China|Tsinghua Univ Dept Energy & Power Engn Beijing 10084 Peoples R China;

    Harbin Inst Technol Sch Energy Sci & Engn Haerbin 150001 Heilongjiang Peoples R China;

    Tsinghua Univ Ctr Combust Energy Beijing 10084 Peoples R China|Tsinghua Univ Dept Energy & Power Engn Beijing 10084 Peoples R China;

    Tsinghua Univ Ctr Combust Energy Beijing 10084 Peoples R China|Tsinghua Univ Dept Energy & Power Engn Beijing 10084 Peoples R China;

    Tsinghua Univ Ctr Combust Energy Beijing 10084 Peoples R China|Tsinghua Univ Dept Energy & Power Engn Beijing 10084 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Surrogate fuel; Pyrolysis curve; Jet fuel; Combustion reaction mechanism;

    机译:替代燃料;热解曲线;喷射燃料;燃烧反应机制;

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