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High-temperature laminar flame speed measurements in a shock tube

机译:电击管中的高温层压火焰速度测量

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摘要

High-temperature methane and propane laminar flame speed measurements were conducted behind reflected shock waves in a shock tube. A high-power Nd:YAG laser was used to spark-ignite the shock-heated gas mixtures and initiate laminar flame propagation. High-speed, OH* endwall imaging was used to record the propagation of the spherically expanding flames in time, and a non-linear stretch correlation was applied and used to determine the unburned, unstretched laminar flame speed. "Low-temperature" (600 K) flame speed results are presented for stoichiometric methane/air and propane/air mixtures at initial unburned gas conditions of 489-573 K and 391-556 K, respectively, and 1 atm. The low-temperature measurements show close agreement with available literature data and kinetic modeling results, thereby validating the shock-tube laminar flame speed measurement approach. "High-temperature" (750 K) flame speed results are presented for a propane/21% O-2-47% N-2-32% He mixture (phi = 0.8) at initial unburned gas conditions of 764-832 K, 1 atm. The high-temperature measurements fall between kinetic model predictions, but the kinetic model results show significant disagreement, highlighting the need for high-temperature flame speed validation data of this kind. We believe that these results represent the first laminar flame speed measurements conducted in a shock tube, and that the high-temperature results are the highest-temperature, 1-atm flame speed measurements available in the literature. (C) 2019 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:高温甲烷和丙烷层状火焰速度测量在反射管中的反射冲击波后面进行。高功率Nd:YAG激光器用于火花 - 点燃冲击加热的气体混合物并引发层状火焰繁殖。使用高速,OH *端壁成像用于记录正方形膨胀火焰的传播及时,并施加非线性拉伸相关性并用于确定未燃烧的未拉伸的层状火焰速度。为489-573k和391-556 k的初始未燃烧的气体条件下,提供了化学计量甲烷/空气和丙烷/空气混合物的化学计量甲烷/空气和丙烷/空气混合物的“低温”(<600 k)的火焰速度结果。低温测量表现出与可用文献数据和动力学建模结果密切一致,从而验证了冲击管层压火焰速度测量方法。 “高温”(> 750K)火焰速度结果在初始未燃烧的气体条件下呈现出丙烷/ 21%O-2-47%N-2-32%HE 2-2-2-47%N-2-32%HE-2-32%,在764-832 k ,1个atm。高温测量落在动力学模型预测之间,但动力学模型结果显示出显着的分歧,突出了对这种高温火焰速度验证数据的需求。我们认为,这些结果表示在冲击管中进行的第一层速度测量,并且高温结果是文献中可用的最高温度,1-ATM火焰速度测量。 (c)2019燃烧研究所。由elsevier Inc.出版的所有权利保留。

著录项

  • 来源
    《Combustion and Flame》 |2019年第7期|241-252|共12页
  • 作者单位

    Stanford Univ Dept Mech Engn 452 Escondido Mall Bldg 520 Stanford CA 94305 USA;

    Stanford Univ Dept Mech Engn 452 Escondido Mall Bldg 520 Stanford CA 94305 USA;

    Stanford Univ Dept Mech Engn 452 Escondido Mall Bldg 520 Stanford CA 94305 USA;

    Stanford Univ Dept Mech Engn 452 Escondido Mall Bldg 520 Stanford CA 94305 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

    Laminar flame speed; Laser-induced spark ignition; Propane; Methane; Shock tube;

    机译:层状火焰速度;激光诱导的火花点火;丙烷;甲烷;震动管;

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