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The effects of sooting in droplet combustion under microgravity and normal-gravity conditions.

机译:在微重力和正重力条件下烟droplet燃烧中烟so的影响。

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摘要

It is recognized that individual droplet behavior is a necessary component for laying the foundation for a better understanding of spray processes. Under the idealized situation producing spherically-symmetric flames, it represents the simplest geometry in which to formulate and solve the governing equations of mass, species and heat transfer for a chemically reacting two-phase flow with phase change. However, most fundamental studies of droplet combustion have not considered sooting effects which have impeded the development of useful strategies for particulate emission control.;As part of this study, the effects of sooting in droplet combustion under microgravity conditions were investigated using the 2.2 second droptower at NASA-Lewis Research Center. The distributions of the soot volume fraction and the flame temperatures were measured using full-field light extinction and the two-wavelength pyrometry techniques, respectively. This represents the first measurements of soot concentrations under microgravity conditions for a spherically-symmetric droplet flame. Results indicate that the soot concentrations for microgravity flames were significantly higher than corresponding values measured for normal-gravity flames. It is believed that this is caused by the longer residence times and thermophoretic effects that are manifested under microgravity condition.;Burning rate and soot volume fraction measurements which were performed for various-sized droplets indicate that the maximum soot volume fraction and the mass of soot contained within the region bounded by the droplet surface and the luminous flame increase significantly as droplet diameter is increased. The presence of the soot particles within this region can modify the effective thermophysical properties. It was also demonstrated that radiative heat losses may account for the observed reductions in the burning rate as the droplet size was increased.;The pressure reduction experiments demonstrated that the soot volume fraction is sensitive to the ambient pressure. At 1 atm, the average soot volume fraction was ;In the normal-gravity experiments, the soot volume fraction for toluene flames was measured using full-field light extinction/tomographic inversion. Experiments performed using simultaneous gravimetric sampling and full-field light extinction indicate a direct relationship between soot volume fraction and the total soot yield. The calibrated optical technique can be used for simultaneously measuring the detailed structure of the sooting region within the flame and for measuring the total soot emitted to the environment in a non-intrusive manner.
机译:公认的是,各个液滴行为是为更好地理解喷涂过程奠定基础的必要组成部分。在产生球形对称火焰的理想情况下,它代表了最简单的几何形状,在该几何形状中,公式化并求解了具有相变的化学反应两相流的质量,种类和热传递的控制方程式。但是,大多数液滴燃烧的基础研究并未考虑烟灰效应,这阻碍了控制颗粒物排放的有效策略的发展。作为这项研究的一部分,使用2.2秒的滴水塔研究了微重力条件下烟灰燃烧对烟尘的影响。在NASA-刘易斯研究中心。烟灰体积分数和火焰温度的分布分别使用全场消光和两波长高温法测量。这代表了在球形重力液滴火焰的微重力条件下烟尘浓度的首次测量。结果表明,微重力火焰的烟灰浓度显着高于正重力火焰测得的相应值。据信这是由于在微重力条件下表现出的更长的停留时间和热泳效应所引起的。对各种大小的液滴进行的燃烧率和烟灰体积分数测量表明最大的烟灰体积分数和烟灰质量。随着液滴直径的增加,包含在由液滴表面和发光火焰所界定的区域内的杂质显着增加。在该区域内烟灰颗粒的存在可以改变有效的热物理性质。还表明,随着液滴尺寸的增加,辐射热损失可能是观察到的燃烧速率下降的原因。降压实验表明,烟灰体积分数对环境压力敏感。在1个大气压下,平均烟灰体积分数为;在正常重力实验中,使用全场光消光/断层扫描法测量甲苯火焰的烟灰体积分数。使用同时进行的重量采样和全场消光进行的实验表明,烟灰体积分数与总烟灰产量之间存在直接关系。校准的光学技术可用于同时测量火焰内烟ing区域的详细结构,并用于以非侵入方式测量排放到环境中的烟灰总量。

著录项

  • 作者

    Lee, Kyeong-Ook.;

  • 作者单位

    University of Illinois at Chicago.;

  • 授予单位 University of Illinois at Chicago.;
  • 学科 Engineering Aerospace.;Engineering Automotive.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 166 p.
  • 总页数 166
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 遥感技术;
  • 关键词

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