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An experimental and modeling study of propene oxidation. Part 2: Ignition delay time and flame speed measurements

机译:丙烯氧化的实验和模型研究。第2部分:点火延迟时间和火焰速度测量

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摘要

Experimental data obtained in this study (Part Ⅱ) complement the speciation data presented in Part Ⅰ, but also offer a basis for extensive facility cross-comparisons for both experimental ignition delay time (IDT) and laminar flame speed (LFS) observables. To improve our understanding of the ignition characteristics of propene, a series of IDT experiments were performed in six different shock tubes and two rapid compression machines (RCMs) under conditions not previously studied. This work is the first of its kind to directly compare ignition in several different shock tubes over a wide range of conditions. For common nominal reaction conditions among these facilities, cross-comparison of shock tube IDTs suggests 20-30% reproducibility (2σ) for the IDT observable. The combination of shock tube and RCM data greatly expands the data available for validation of propene oxidation models to higher pressures (2-40 atm) and lower temperatures (750-1750 K). Propene flames were studied at pressures from 1 to 20 atm and unburned gas temperatures of 295-398 K for a range of equivalence ratios and dilutions in different facilities. The present propene-air LFS results at 1 atm were also compared to LFS measurements from the literature. With respect to initial reaction conditions, the present experimental LFS cross-comparison is not as comprehensive as the IDT comparison; however, it still suggests reproducibility limits for the LFS observable. For the LFS results, there was agreement between certain data sets and for certain equivalence ratios (mostly in the lean region), but the remaining discrepancies highlight the need to reduce uncertainties in laminar flame speed experiments amongst different groups and different methods. Moreover, this is the first study to investigate the burning rate characteristics of propene at elevated pressures (>5 atm). IDT and LFS measurements are compared to predictions of the chemical kinetic mechanism presented in Part Ⅰ and good agreement is observed.
机译:本研究(第二部分)获得的实验数据补充了第一部分中提供的形态数据,但也为可观察到的实验点火延迟时间(IDT)和层流火焰速度(LFS)的广泛设施交叉比较提供了基础。为了增进我们对丙烯着火特性的理解,在先前未研究的条件下,在六个不同的冲击管和两个快速压缩机(RCM)中进行了一系列IDT实验。这项工作是在广泛的条件下直接比较几种不同的冲击管点火的同类研究中的第一项。对于这些设施中常见的标称反应条件,冲击管IDT的交叉比较表明,可观察到的IDT具有20-30%的重现性(2σ)。冲击管和RCM数据的结合极大地扩展了可用于验证丙烯氧化模型的数据,使其适用于更高的压力(2-40 atm)和更低的温度(750-1750 K)。对丙烯火焰进行了研究,压力范围为1至20个大气压,未燃烧的气体温度为295-398 K,适用于不同设施中的当量比范围和稀释度。还将目前在1个大气压下的丙烯空气LFS结果与文献中的LFS测量结果进行了比较。关于初始反应条件,目前的实验性LFS交叉比较不如IDT比较全面。但是,它仍然建议可观察到的LFS的再现性极限。对于LFS结果,某些数据集和某些当量比(主要在稀薄区域)之间是一致的,但是其余差异突出显示了需要减少不同组和不同方法之间的层流火焰速度实验​​的不确定性。此外,这是第一个研究在高压(> 5 atm)下丙烯燃烧速率特性的研究。将IDT和LFS的测量结果与第一部分所述的化学动力学机理的预测结果进行了比较,并观察到了很好的一致性。

著录项

  • 来源
    《Combustion and Flame》 |2015年第2期|296-314|共19页
  • 作者单位

    Combustion Chemistry Centre, National University of Ireland, Galway, Ireland;

    Combustion Chemistry Centre, National University of Ireland, Galway, Ireland;

    Combustion Chemistry Centre, National University of Ireland, Galway, Ireland;

    Department of Mechanical Engineering, Texas A&M University, College Station, TX, United States;

    Department of Mechanical Engineering, Texas A&M University, College Station, TX, United States;

    Department of Mechanical Engineering, Texas A&M University, College Station, TX, United States;

    Department of Mechanical Engineering, Texas A&M University, College Station, TX, United States;

    Department of Mechanical Engineering, Texas A&M University, College Station, TX, United States;

    Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY, United States;

    Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY, United States;

    Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY, United States;

    Department of Mechanical Engineering, Stanford University, CA, United States;

    Department of Mechanical Engineering, Stanford University, CA, United States;

    Department of Mechanical Engineering, Stanford University, CA, United States;

    Department of Mechanical Engineering, University of Connecticut, CT, United States;

    Department of Mechanical Engineering, University of Connecticut, CT, United States;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ, United States;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ, United States;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ, United States;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ, United States;

    Technical University of Eindhoven, Eindhoven, The Netherlands;

    Division of Combustion Physics, Lund University, Lund, Sweden;

    Division of Combustion Physics, Lund University, Lund, Sweden;

    Clean Combustion Research Center, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia;

    Clean Combustion Research Center, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia;

    Clean Combustion Research Center, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia;

    Laboratoire Reactions et Genie des Procedes, CNRS-Universite de Lorraine, Nancy, France;

    Laboratoire Reactions et Genie des Procedes, CNRS-Universite de Lorraine, Nancy, France;

    Laboratoire Reactions et Genie des Procedes, CNRS-Universite de Lorraine, Nancy, France;

    Combustion Chemistry Centre, National University of Ireland, Galway, Ireland;

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

    Propene oxidation; Shock tube; Rapid compression machine; Chemical kinetics; Ignition; Flame speed;

    机译:丙烯氧化;避震管;快速压缩机;化学动力学;点火;火焰速度;
  • 入库时间 2022-08-18 00:11:06

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