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Ignition of n-heptane pool by heated stagnating oxidizing flow

机译:通过加热停滞氧化流点燃正庚烷池

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摘要

The ignition temperature of a liquid pool of n-heptane by heated oxidizer in a stagnation flow was experimentally determined for system pressures of 0.61-3 atm and pressure-weighted strain rates of 60-350 s~(-1). The surface of the liquid pool was maintained at a fixed location through continuous replenishment. The state of ignition was brought about, and monitored, by gradually increasing the oxidizer temperature. The strain rate was determined by seeding and measuring the oxidizer flow velocity using laser Doppler velocimetry (LDV).rnComputational simulation of the ignition event with detailed chemistry and transport was conducted by using a stagnation-flow code. The kinetic mechanisms utilized are a high-temperature n-heptane oxidation model, with 130 species and 955 reactions, and a reduced one of 58 species derived from a detailed mechanism of 561 species and 2539 reactions. The former mechanism yielded better agreement with the experimental measurements in general over the conditions examined. It was also found that the mole fraction of n-heptane at the interface changed only slightly with pressure and strain rate, and can be considered to have minimal effect on the ignition responses studies herein. A recently developed explosive mode analysis (EMA) was conducted to identify the controlling radicals and reactions in the non-pre-mixed ignition of n-heptane.
机译:实验确定了系统温度为0.61-3 atm,压力加权应变率为60-350 s〜(-1)时,在停滞气流中通过加热的氧化剂对正庚烷液池的着火温度进行了实验确定。通过连续补充,将液体池的表面保持在固定位置。通过逐渐提高氧化剂温度来引起并监测着火状态。通过使用激光多普勒测速仪(LDV)播种并测量氧化剂的流速来确定应变率。使用停滞流代码对着火事件进行详细的化学反应和运输的计算模拟。所用的动力学机制是具有130种和955个反应的高温正庚烷氧化模型,以及从561种和2539个反应的详细机理推导的58种减少的一种。在检查的条件下,前者的机理与实验测量结果更好地吻合。还发现界面处的正庚烷的摩尔分数仅随压力和应变率而轻微变化,并且可以认为对本文的点火响应研究影响最小。进行了最近开发的爆炸模式分析(EMA),以识别正庚烷非预混点火中的控制自由基和反应。

著录项

  • 来源
    《Combustion and Flame》 |2010年第2期|259-266|共8页
  • 作者单位

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    ignition; stagnation flow; n-heptane oxidation; explosive mode analysis;

    机译:点火;滞流正庚烷氧化;爆炸模式分析;
  • 入库时间 2022-08-18 00:12:23

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