首页> 外文期刊>Combustion and Flame >Explosion bomb measurements of ethanol-air laminar gaseous flame characteristics at pressures up to 1.4 MPa
【24h】

Explosion bomb measurements of ethanol-air laminar gaseous flame characteristics at pressures up to 1.4 MPa

机译:压力高达1.4 MPa的乙醇-空气层流气态火焰特性的爆炸弹测量

获取原文
获取原文并翻译 | 示例
           

摘要

The principal burning characteristics of a laminar flame comprise the fuel vapour pressure, the laminar burning velocity, ignition delay times, Markstein numbers for strain rate and curvature, the stretch rates for the onset of flame instabilities and of flame extinction for different mixtures. With the exception of ignition delay times, measurements of these are reported and discussed for ethanol-air mixtures. The measurements were in a spherical explosion bomb, with central ignition, in the regime of a developed stable, flame between that of an under or over-driven ignition and that of an unstable flame. Pressures ranged from 0.1 to 1.4 MPa, temperatures from 300 to 393 K, and equivalence ratios were between 0.7 and 1.5. It was important to ensure the relatively large volume of ethanol in rich mixtures at high pressures was fully evaporated. The maximum pressure for the measurements was the highest compatible with the maximum safe working pressure of the bomb. Many of the flames soon became unstable, due to Darrieus-Landau and thermo-diffusive instabilities. This effect increased with pressure and the flame wrinkling arising from the instabilities enhanced the flame speed. Both the critical Peclet number and the, more rational, associated critical Karlovitz stretch factor were evaluated at the onset of the instability. With increasing pressure, the onset of flame instability occurred earlier. The measured values of burning velocity are expressed in terms of their variations with temperature and pressure, and these are compared with those obtained by other researchers. Some comparisons are made with the corresponding properties for iso-octane-air mixtures.
机译:层流火焰的主要燃烧特性包括燃料蒸气压,层流燃烧速度,点火延迟时间,应变率和曲率的马克斯坦数,火焰不稳定和不同混合物的火焰熄灭的拉伸速率。除了点火延迟时间外,还报告并讨论了乙醇-空气混合物的测量方法。测量是在带有中心点火的球形爆炸弹中进行的,其稳定的火焰处于欠驱动或过驱动点火与不稳定火焰之间。压力范围从0.1到1.4 MPa,温度从300到393 K,当量比在0.7到1.5之间。确保高压下浓混合物中相对大量的乙醇完全蒸发非常重要。测量的最大压力与炸弹的最大安全工作压力最高。由于Darrieus-Landau和热扩散不稳定性,许多火焰很快变得不稳定。这种作用随着压力的增加而增加,由不稳定性引起的火焰起皱提高了火焰速度。不稳定开始时,评估了临界Peclet数和更合理的关联临界Karlovitz拉伸因子。随着压力的增加,火焰不稳定性的发生较早发生。燃烧速度的测量值用它们随温度和压力的变化表示,并将其与其他研究人员获得的结果进行比较。对异辛烷-空气混合物的相应性质进行了一些比较。

著录项

  • 来源
    《Combustion and Flame》 |2009年第7期|1462-1470|共9页
  • 作者单位

    School of Mechanical Engineering, University of Leeds, Leeds LS2 9JT, United Kingdom;

    School of Mechanical Engineering, University of Leeds, Leeds LS2 9JT, United Kingdom;

    School of Mechanical Engineering, University of Leeds, Leeds LS2 9JT, United Kingdom;

  • 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

    ethanol burning velocities; markstein numbers; critical flame instability data; explosions;

    机译:乙醇燃烧速度;马克斯坦数临界火焰不稳定性数据;爆炸;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号