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Measurements and interpretation of shock tube ignition delay times in highly CO2 diluted mixtures using multiple diagnostics

机译:使用多种诊断程序测量和解释高CO2稀释混合物中冲击管点火延迟时间

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摘要

Common definitions for ignition delay time are often hard to determine due to the issue of bifurcation and other non-idealities that result from high levels of CO2 addition. Using high-speed camera imagery in comparison with more standard methods (e.g., pressure, emission, and laser absorption spectroscopy) to measure the ignition delay time, the effect of bifurcation has been examined in this study. Experiments were performed at pressures between 0.6 and 1.2 atm for temperatures between 1650 and 2040 K. The equivalence ratio for all experiments was kept at a constant value of 1 with methane as the fuel. The CO2 mole fraction was varied between a value of)(co, = 0.00 to 0.895. The ignition delay time was determined from three different measurements at the sidewall: broadband chemiluminescent emission captured via a photodetector, CH84 concentrations determined using a distributed feedback interband cascade laser centered at 3403.4 nm, and pressure recorded via a dynamic Kistler type transducer. All methods for the ignition delay time were compared to high-speed camera images taken of the axial cross-section during combustion. Methane time-histories and the methane decay times were also measured using the laser. It was determined that the flame could be correlated to the ignition delay time measured at the side wall but that the flame as captured by the camera was not homogeneous as assumed in typical shock tube experiments. The bifurcation of the shock wave resulted in smaller flames with large boundary layers and that the flame could be as small as 30% of the cross-sectional area of the shock tube at the highest levels of CO2 dilution. Comparisons between the camera images and the different ignition delay time methods show that care must be taken in interpreting traditional ignition delay data for experiments with large bifurcation effects as different methods in measuring the ignition delay time could result in different interpretations of kinetic mechanisms and impede the development of future mechanisms. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:点火延迟时间的通用定义通常难以确定,这是由于分叉问题和高添加CO2导致的其他不理想的问题。与其他标准方法(例如压力,发射和激光吸收光谱法)相比,使用高速相机成像来测量点火延迟时间,在此研究中检查了分叉的影响。在1650至2040 K之间的温度下,在0.6至1.2 atm的压力下进行了实验。使用甲烷作为燃料,所有实验的当量比均保持恒定值1。 CO2摩尔分数在(co,= 0.00至0.895)值之间变化。点火延迟时间由侧壁的三个不同测量值确定:通过光电探测器捕获的宽带化学发光发射,使用分布反馈带间级联确定CH84浓度激光以3403.4 nm为中心,并通过动态Kistler型传感器记录压力,将所有点火延迟时间的方法与燃烧过程中轴向横截面的高速相机图像进行了比较,甲烷的时间历史和甲烷的衰减时间还确定了火焰可以与在侧壁上测量到的点火延迟时间相关联,但是相机捕获的火焰并不像典型的冲击管实验所假定的那样均匀。冲击波产生的火焰较小,边界层较大,并且火焰可能小至t的横截面积的30%在最高浓度的CO2稀释下使电击管破裂。摄像机图像与不同点火延迟时间方法之间的比较表明,对于分叉效应较大的实验,在解释传统点火延迟数据时必须格外小心,因为测量点火延迟时间的不同方法可能会导致对动力学机理的不同解释,并阻碍发展未来的机制。 (C)2017燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

  • 来源
    《Combustion and Flame》 |2017年第6期|63-76|共14页
  • 作者单位

    Univ Cent Florida, CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA;

    Univ Cent Florida, CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA;

    Univ Cent Florida, CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA|Lawrence Livermore Natl Lab, Livermore, CA 94550 USA;

    Univ Cent Florida, CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA;

    Univ Cent Florida, CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA;

  • 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

    CO2; Shock tube; Bifurcation; Ignition delay time; Chemical kinetics;

    机译:二氧化碳;冲击管;分叉;点火延迟时间;化学动力学;

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