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Microgravity studies of methanol droplet combustion.

机译:甲醇液滴燃烧的微重力研究。

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摘要

The objective of this work is to investigate the structure and flame extinction of methanol droplets burning in air. Asymptotic methods are employed to describe the flame structure and extinction of quasisteady, spherically symmetrical diffusion flames around methanol droplets. Starting with a short mechanism involving fourteen steps, sequentially reduced overall descriptions of four, three and two steps are obtained by investigating the character of the departure of the H atom and its associated radicals from steady states and by demonstrating that, contrary to hydrocarbon flames, water-gas equilibrium is an excellent approximation in the reaction zones of these methanol flames. It is shown that a useful two-step approximation is described qualitatively by ;Unlike alkane droplet combustion, methanol is completely miscible with water. Interactions between the vaporization and combustion processes of methanol involve fairly complicated transport and flow phenomena. A time-dependent model with water absorption and re-evaporation has been introduced and developed by employing quasisteady gas-phase analysis with non-unity Lewis number for water, unity Lewis numbers for other species. By coupling with asymptotic analysis, this method yields a formulation which eliminates the transport effects, that is, the dependence of extinction diameter on the initial diameter is a thermodynamic and chemical-kinetic property. The perfect mixing model predicted that for methanol droplets burning in air, the extinction diameter increases linearly with the initial diameter. This linear relationship was confirmed later by the USML-2 space experiment. Reasonable agreement with theoretically reported extinction diameters, obtained from detailed time-dependent computations and from USML-2 space mission Fiber Supported Droplet Combustion experiments, is thereby achieved by including about 20% initial water absorption before droplet ignition in the theoretical model. The results provide an analytical method for calculating methanol droplet combustion and extinction.
机译:这项工作的目的是研究在空气中燃烧的甲醇液滴的结构和火焰熄灭。渐近方法用于描述甲醇液滴周围的准稳固球形对称扩散火焰的火焰结构和熄灭。从涉及14个步骤的简短机制开始,通过研究H原子及其相关自由基从稳态离开的特性并证明与碳氢化合物火焰相反,依次减少了对4、3和2个步骤的总体描述。在这些甲醇火焰的反应区中,水-气平衡非常好。结果表明,定性描述了一个有用的两步近似;与烷烃滴燃烧不同,甲醇与水完全混溶。甲醇的汽化和燃烧过程之间的相互作用涉及相当复杂的运输和流动现象。通过采用准稳态气相分析引入水的吸收和再蒸发的时间相关模型,其中水的非路易斯值统一,其他物种的路易斯值统一。通过与渐近分析相结合,该方法产生了一种消除运输效应的配方,即消光直径对初始直径的依赖性是热力学和化学动力学性质。完美的混合模型预测,对于在空气中燃烧的甲醇小滴,消光直径会随着初始直径线性增加。此线性关系随后由USML-2空间实验确认。通过详细的时变计算和USML-2太空任务纤维支持的液滴燃烧实验获得的与理论上记录的消光直径的合理一致,从而通过在理论模型中包括约20%的液滴点燃前的初始吸水率来实现。该结果提供了一种计算甲醇滴燃烧和消光的分析方法。

著录项

  • 作者

    Zhang, Baili.;

  • 作者单位

    University of California, San Diego.;

  • 授予单位 University of California, San Diego.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 82 p.
  • 总页数 82
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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