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An experimental and computational study on the propagation and kinetic structure of laminar premixed flames.

机译:层流预混火焰传播和动力学结构的实验和计算研究。

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摘要

The steady propagation and chemical kinetic structure of adiabatic, planar, laminar premixed flames were experimentally and numerically studied with systematic and extensive variations of the effects of fuel, oxidizer, pressure, stoichiometry, and flame temperature. Experimentally, the laminar flame speeds were determined by using the counterflow twin-flame configuration, with laser Doppler velocimetry probing and systematic elimination of flame stretch effects. Numerical simulation was conducted by using validated hydro and transport codes together with various detailed chemical kinetic mechanisms. The parameter matrix of investigation included H{dollar}sb2{dollar}, CO, CH{dollar}sb4{dollar}, all C{dollar}sb2{dollar}-hydrocarbons, and C{dollar}sb3{dollar}H{dollar}sb8{dollar} as fuels, He, Ar, N{dollar}sb2{dollar}, and CO{dollar}sb2{dollar} as inert diluents, pressure variations from 0.2 to 4.5 atmospheres, stoichiometry from very fuel lean to very fuel rich, and flame temperature from 1550 to 2250 K varied independently of stoichiometry.; Results on methane flames clearly demonstrate the importance of branching-termination chain mechanisms on flame propagation. The pressure exponent n for the overall mass burning rate of the flame is shown to continuously decrease with pressure while the corresponding overall activtion energy continuously increases. For weakly-burning flames n can even assume negative values, indicating decreasing mass burning rates with increasing pressure.; Results on mixtures of ethane, ethylene, acetylene, and propane with oxygen and nitrogen show the inadequacies of all literature kinetic schemes in predicting the experimental flame speed. Consequently, a new scheme was compiled and was found to yield close agreement with the majority of the experimental data.; The study of hydrogen flames emphasizes on the role of high-, intermediate-, and low-temperature regime kinetics on the flame response. Results show that while literature kinetic schemes accurately predict the propagation rates of high temperature flames, they seriously underpredict those of low-temperature flames.; An independent study of the phenomena of flammability limits was conducted. Experimentally, limits of propagation of unstretched flames were determined by first measuring the extinction limits of stretched, counterflow flames and extrapolating the results to zero stretch. Consequently, lean and rich flammability limits were determined for a large variety of mixtures. By further hypothesizing that the limit phenomena are primarily controlled by the kinetic processes of chain branching versus termination, a predictive theory was advanced for the a priori determination of flammability limits. Calculated limits largely agree with the experimentally-determined values.
机译:对绝热,平面,层流预混火焰的稳态传播和化学动力学结构进行了实验和数值研究,对燃料,氧化剂,压力,化学计量和火焰温度的影响进行了系统且广泛的变化。实验上,层流火焰速度是通过使用逆流双火焰配置,激光多普勒测速仪探测和系统消除火焰拉伸效应来确定的。通过使用经过验证的水力和运输代码以及各种详细的化学动力学机理进行了数值模拟。研究的参数矩阵包括H {dolb} sb2 {dollar},CO,CH {dollar} sb4 {dollar},所有C {dollar} sb2 {dollar}-碳氢化合物和C {dollar} sb3 {dollar} H {dollar } sb8 {dollar}作为燃料,He,Ar,N {dollar} sb2 {dollar}和CO {dollar} sb2 {dollar}作为惰性稀释剂,压力从0.2到4.5个大气压变化,化学计量从非常稀的燃料到非常稀的燃料;火焰温度从1550到2250 K不依赖于化学计量。甲烷火焰的结果清楚地表明了分支终止链机制对火焰传播的重要性。火焰总质量燃烧速率的压力指数n随压力不断降低,而相应的总活化能则不断增加。对于弱燃烧的火焰,n甚至可以取负值,表明随着压力的增加,质量燃烧速率降低。乙烷,乙烯,乙炔和丙烷与氧气和氮气的混合物的结果表明,所有文献动力学方案均不足以预测实验火焰速度。因此,一个新的方案被编译并被发现与大多数实验数据有着紧密的一致性。氢火焰的研究强调了高温,中温和低温状态动力学对火焰响应的作用。结果表明,尽管文献动力学方案能够准确预测高温火焰的传播速率,但它们严重低估了低温火焰的传播速率。对可燃性极限现象进行了独立研究。实验上,通过首先测量拉伸的逆流火焰的消光极限并将结果外推到零拉伸,来确定未拉伸火焰的传播极限。因此,确定了多种混合物的稀薄和浓燃性极限。通过进一步假设极限现象主要受链支化与终止动力学过程的控制,提出了一种可预测性理论,用于事先确定可燃性极限。计算的极限值与实验确定的值基本吻合。

著录项

  • 作者

    Egolfopoulos, Fokion.;

  • 作者单位

    University of California, Davis.;

  • 授予单位 University of California, Davis.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1990
  • 页码 209 p.
  • 总页数 209
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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