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Numerical study on vaporization and burning of multi-component stationary fuel droplets and single-component convective fuel droplets both with complex configuration and variable properties.

机译:具有复杂结构和可变特性的多组分固定燃料液滴和单组分对流燃料液滴的蒸发和燃烧的数值研究。

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摘要

The studies of droplets and sprays have important applications in many combustors. In the study of stationary droplets, an analysis is presented for multicomponent-liquid-fuel vaporization in a general geometrical situation for non-unitary Lewis number. Variable transport properties and only Stefan flow are considered. The problem becomes a one-dimensional problem for the quasi-steady gas-phase scalar properties by using a mass-flux potential function. Transient heat and mass diffusion in the liquid interiors is considered with special attention given to the fast- and slow-diffusion limits. Eight droplets in a cubic array are considered in the calculations with a blended liquid mixture of heptane, octane, and decane. Comparisons are made amongst the results for the various liquid-diffusion models: transient behavior, the fast vaporization limit, and the slow vaporization limit.;In the studies of convecting droplets, the transient burning of fuel droplets in a hot gas stream is numerically investigated by solving the Navier-Stokes, energy and species equations. Droplet surface regression, deceleration of the stream flow due to the drag on the droplet, internal circulation inside the droplet, variable properties, non-uniform surface temperature, and the effect of surface tension are considered. The array configurations examined in these studies include an isolated droplet, single-layer droplet arrays (infinite periodic arrays, semi-infinite periodic arrays with one row or two rows of droplets, and finite arrays with nine droplets with centers in a plane), and infinite periodic arrays with two layers of droplets. The transient flame shape, surface temperature, burning rate, and dimensionless numbers are studied for different array configurations, initial droplet spacing (for multi-droplet cases), initial droplet radius, initial Reynolds number, initial Damkohler number, and ambient conditions including ambient pressure, temperature and oxygen concentration. Particularly, the critical parameters for the determination of the initial flame shapes, the flame transition (from a wake flame to an envelope flame) time and its influence on the burning rate are determined. Both overall one-step chemical kinetics and four-step reduced chemical mechanism are used to account for the gas-phase combustion in the calculation for an isolated droplet, in order to study the differences in the results introduced from the improved chemical kinetics. In the multi-droplet calculation, only one-step chemical kinetics is used.
机译:液滴和喷雾的研究在许多燃烧器中都有重要的应用。在固定液滴的研究中,对非analysis路易斯数的一般几何条件下的多组分液体燃料汽化进行了分析。可变的传输特性和仅Stefan流被考虑。通过使用质量通量势函数,该问题成为准稳态气相标量特性的一维问题。考虑到液体内部的瞬态热和质量扩散,要特别注意快速和慢速扩散极限。计算中考虑了庚烷,辛烷和癸烷的混合液体混合物中立方阵列中的八个液滴。在各种液体扩散模型的结果之间进行了比较:瞬态行为,快速汽化极限和慢速汽化极限。;在对流液滴的研究中,对热气流中燃料液滴的瞬时燃烧进行了数值研究。通过求解Navier-Stokes,能量和物种方程。考虑了液滴表面回归,由于液滴上的阻力而引起的水流的减速,液滴内部的内部循环,可变的特性,不均匀的表面温度以及表面张力的影响。在这些研究中检查的阵列配置包括隔离液滴,单层液滴阵列(无限周期阵列,具有一排或两行液滴的半无限周期阵列,以及在平面内有九个液滴的有限阵列),以及具有两层液滴的无限周期阵列。研究了瞬态火焰形状,表面温度,燃烧速率和无因次数,适用于不同的阵列配置,初始液滴间距(对于多液滴情况),初始液滴半径,初始雷诺数,初始Damkohler数以及包括环境压力在内的环境条件,温度和氧气浓度。特别地,确定用于确定初始火焰形状,火焰过渡(从尾焰到包络火焰)时间及其对燃烧速率的影响的关键参数。整体的一步化学动力学和四步简化的化学机理都用于计算孤立液滴的气相燃烧,以研究改进的化学动力学引入的结果差异。在多液滴计算中,仅使用一步化学动力学。

著录项

  • 作者

    Wu, Guang.;

  • 作者单位

    University of California, Irvine.;

  • 授予单位 University of California, Irvine.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 210 p.
  • 总页数 210
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:45:40

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