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Experimental Investigation on Laminar Burning Velocities and Markstein Lengths of Premixed Methane-n-Heptane-Air Mixtures

机译:预混合甲烷-正庚烷-空气混合物的层流燃烧速度和马克斯坦长度的实验研究

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摘要

Laminar burning velocities and Markstein lengths of premixed methane-n-heptane-air mixtures were experimentally investigated at an initial pressure of 0.1 MPa, initial temperatures of 358, 393, and 428 K, and equivalence ratios of 0.7-1.5. The methane content in the methane-n-heptane mixtures ranges from 0 to 1. The experiments were conducted in a combustion chamber with central ignition. In the present study, the difference between the linear and nonlinear extrapolation methods was analyzed quantitatively for methane-n-heptane air flames. Comparisons of the laminar burning velocities of methane-air and n-heptane-air flames were conducted, respectively, between the present and other studies. Subsequently, effects of the initial temperature and methane content on the laminar burning velocity and flame instability of methane n-heptane air mixtures were analyzed. Then, the critical methane content at which the laminar burning velocity and flame instability of methane n-heptane air flames start to change relatively significantly was explored. The results show that the laminar burning velocities of methane air and n-heptane air flames measured in the present study are in good agreement with the data available in the literature. Laminar burning velocities and flame instabilities of methane n-heptane air flames seem to be less sensitive to the methane content when the methane content is below 0.75. The change in the initial temperature tends to diminish the difference in the laminar burning velocity between methane air and n-heptane air flames and only has weak effects on the flame instability of methane-n-heptane air mixtures. According to variations of the laminar burning velocities and Markstein lengths of methane n-heptane-air flames with the methane content, the value of 0.75 can be treated preliminarily as the critical methane content.
机译:在0.1 MPa的初始压力,358、393和428 K的初始温度以及0.7-1.5的当量比的条件下,通过实验研究了预混合的甲烷-正庚烷-空气混合物的层流燃烧速度和Markstein长度。甲烷-正庚烷混合物中的甲烷含量为0至1。实验在带有中央点火装置的燃烧室中进行。在本研究中,定量分析了甲烷-正庚烷空气火焰的线性和非线性外推方法之间的差异。在本研究与其他研究之间,分别对甲烷-空气和正庚烷-空气火焰的层流燃烧速度进行了比较。随后,分析了初始温度和甲烷含量对甲烷正庚烷混合气层流燃烧速度和火焰不稳定性的影响。然后,研究了甲烷正庚烷空气层流燃烧速度和火焰不稳定性开始显着变化的临界甲烷含量。结果表明,在本研究中测得的甲烷空气和正庚烷空气火焰的层流燃烧速度与文献中的数据非常吻合。当甲烷含量低于0.75时,甲烷正庚烷空气层流的层流燃烧速度和火焰不稳定性似乎对甲烷含量较不敏感。初始温度的变化趋向于减小甲烷空气和正庚烷空气火焰之间的层流燃烧速度的差异,并且仅对甲烷-正庚烷空气混合物的火焰不稳定性具有微弱的影响。根据层流燃烧速度和甲烷正庚烷空气火焰随甲烷含量的马克斯坦长度的变化,可以将0.75的值初步视为临界甲烷含量。

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  • 来源
    《Energy & fuels》 |2015年第julaaauga期|4549-4556|共8页
  • 作者单位

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

    Wuhan Univ Technol, Sch Energy & Power Engn, Key Lab High Performance Ship Technol, Minist Educ, Wuhan 430063, Hubei, Peoples R China;

  • 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
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  • 入库时间 2022-08-18 00:40:17

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