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Detonation in Mixtures of JP-10 Vapor and Air

机译:JP-10蒸气和空气混合物中的爆炸

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摘要

An experimental study of the detonation properties of the high molecular weight aviation fuel JP-10 was performed. Detonation cell size measurements for mixtures of JP-10 vapor and air at elevated initial temperatures are reported. Experiments are preformed in a 6.2-m-long, 10-cm inner-diameter heated detonation tube at an initial mixture pressure of 2 atm and initial temperatures of 373, 473, and 528 K. The first half of the tube is equipped with turbulence producing orifice plates. Flame acceleration leads to detonation initiation within the first 2 m of the orifice-plate-laden part of the tube, and a detonation wave propagates in the smooth second half of the tube. The detonation cellular structure is recorded on a soot foil inserted into the end of the tube. The detonation velocity measured just before the foil is within 1 to 2% of the theoretical Chapman-Jouget velocity. The detonation cellular structure for off-stoichiometric mixtures was found to contain substantial substructure. The average cell size is obtained by measuring the transverse distance between parallel diagonal tracks scoured onto the foil. It was found that to within the measurement uncertainty the cell size changed very little over the temperature range tested. The measured deflagration-to-detonation transition composition limits are found to correlate well with the classical detonation propagation criterion based on the detonation cell size λ and the orifice plate diameter d, that is, d/λ ≥ 1. The measured JP-10 vapor air mixture cell size is correlated with the calculated Zeldovich von Neumann Doring (ZND) induction length for propane air mixtures with similar stoichiometry.
机译:对高分子量航空燃料JP-10的爆炸特性进行了实验研究。报道了在升高的初始温度下JP-10蒸气和空气混合物的爆轰孔尺寸测量。实验是在6.2 m长,内径为10 cm的内爆管中进行的,初始混合压力为2 atm,初始温度为373、473和528K。该管的前半部分装有湍流生产孔板。火焰加速导致在装有孔板的管子的前2 m内引发爆炸,并且在管子的光滑后半部分传播起爆波。爆轰孔结构记录在插入管端的烟灰箔上。箔片之前测得的爆轰速度在理论Chapman-Jouget速度的1-2%之内。发现非化学计量混合物的爆炸孔结构包含大量的亚结构。平均泡孔尺寸是通过测量冲刷到箔片上的平行对角线轨迹之间的横向距离而获得的。发现在测量不确定性范围内,电池尺寸在测试的温度范围内变化很小。基于爆轰孔尺寸λ和孔板直径d,即d /λ≥1,发现测得的爆燃到爆轰过渡成分极限与经典爆轰传播准则非常相关。对于具有相似化学计量比的丙烷空气混合物,空气混合物孔的大小与计算的Zeldovich von Neumann Doring(ZND)诱导长度相关。

著录项

  • 来源
    《AIAA Journal》 |2006年第2期|p.362-367|共6页
  • 作者

    G. Ciccarelli; J. Card;

  • 作者单位

    Queen's University, Kingston, Ontario K7L 3N6, Canada;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天;航空;
  • 关键词

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