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An experimental investigation of flame spreading from bluff body flameholders

机译:钝体火焰稳定器火焰蔓延的实验研究

摘要

Flame spreading from 1/16 to l inch circular cylinder flame holders in two-dimensional flow was studied experimentally. Combustion wake widths were determined by use of spark Schlieren photographs at distances up to 36 inches downstream of the flame-holder in a 3 by 6 inch duct. The effect on wake width and flow parameters of several geometric and operating variables was observed.The data show that above a critical approach gas velocity, corresponding to the transition from laminar to turbulent flow in the flame front, the wake width was independent of velocity and remained constant. Below the critical velocity the wake width was a strong function of velocity. Small but real effects were found on changing fuel-air ratios. The wake width was smallest and the wake spreading rate lowest at the stoichiometric fuel-air ratio. An eight to one variation in flameholder diameter resulted in only a 30 per cent variation in wake width at a distance of one duct height downstream. Farther downstream the variation was even less. Total and static pressure measurements showed that combustion processes fix the total pressure wake and that the losses associated with flameholder drag were not important in fixing the wake spreading rate.
机译:实验研究了二维流动中从1/16火焰扩散到1英寸圆柱火焰的火焰。燃烧尾流宽度是通过使用火花Schlieren照片在3 x 6英寸管道中的火焰保持器下游最多36英寸的距离处确定的。观察到了几个几何和操作变量对尾流宽度和流动参数的影响。数据显示,在临界进场气体速度以上,对应于火焰前部从层流到湍流的过渡,尾流宽度与速度和速度无关。保持不变。在临界速度以下,尾流宽度是速度的强函数。在改变燃料空气比方面发现了很小但真正的影响。在化学计量的燃料空气比下,尾流宽度最小,尾流扩散率最低。火焰保持器直径的八比一变化导致在下游一个导管高度处的尾流宽度仅变化了30%。在更下游,变化甚至更少。总压和静压测量结果表明,燃烧过程固定了总压力尾流,而与火焰保持器阻力相关的损失对确定尾流扩散率并不重要。

著录项

  • 作者

    Thurston Dick W.;

  • 作者单位
  • 年度 1958
  • 总页数
  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
  • 中图分类

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