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首页> 外文期刊>Journal of propulsion and power >Systematic Measurement of Hydrocarbon Fuel Droplet Burning Rate Constants and Ignition Delays
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Systematic Measurement of Hydrocarbon Fuel Droplet Burning Rate Constants and Ignition Delays

机译:烃类燃料液滴燃烧速率常数和点火延迟的系统测量

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摘要

In this experimental study, a new data reduction approach was developed for measuring droplet burning rate constants that automatically finds the most linear part of the d-squared curve for the longest period of time. The approach, here called K beta, was developed in response to the observation that burning rate constants can vary by up to 10%, depending on the reduction approach used, especially for fuel types such as nonvolatile simple hydrocarbons and kerosenes. To evaluate this new method, burning rate constants were measured for 10 fuels, including two alcohols, four simple hydrocarbons and four kerosene blends. The measured rates ranged from 0.74 to 0.94 mm2/s, typically grouped by similarities in thermophysical properties of the fuel types. Notably, K beta and its simpler equivalent Kend,5,70 yielded burning rates with small statistical uncertainty (approximate to 0.006 mm2/s average) across all fuels and were associated with the highest coefficient of determination for all K measurement approaches, indicating that these two methods are viable options for improved consistency in measuring burning rate constants. In addition, a systematic method is presented for measuring ignition delays tau ign using a short-duration plasma source for ignition. The ignition delays ranged from 65 to 110 ms for most fuels, correlating well with the fuel boiling temperature. Combined, this work provides baseline data and data reduction tools suitable for future droplet combustion studies.
机译:在这项实验研究中,开发了一种新的数据缩减方法来测量液滴燃烧速率常数,该方法可在最长的时间内自动找到d平方曲线的最线性部分。响应于观察到的燃烧速率常数最多可变化10%的现象而开发的方法,在此称为K beta,这取决于所使用的还原方法,尤其是对于燃料类型,例如非挥发性简单烃和煤油。为了评估这种新方法,测量了10种燃料的燃烧速率常数,包括两种醇,四种简单烃和四种煤油混合物。测得的速率范围为0.74至0.94 mm2 / s,通常按燃料类型的热物理性质的相似性分组。值得注意的是,K beta及其更简单的当量Kend [5,70]产生的燃烧速率在所有燃料中均具有较小的统计不确定性(平均约为0.006 mm2 / s),并且与所有K测量方法的最高测定系数相关,表明这些两种方法都是可行的选择,可以提高燃烧速率常数的一致性。此外,提出了一种系统的方法,用于使用短时等离子体源进行点火来测量点火延迟tau ign。大多数燃料的点火延迟范围从65到110毫秒,与燃料的沸腾温度密切相关。结合起来,这项工作提供了适用于未来液滴燃烧研究的基准数据和数据减少工具。

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  • 来源
    《Journal of propulsion and power》 |2019年第4期|690-703|共14页
  • 作者单位

    ERC Inc, 10 E Saturn Blvd,Bldg 8451, Edwards AFB, CA 93524 USA;

    ERC Inc, 10 E Saturn Blvd,Bldg 8451, Edwards AFB, CA 93524 USA;

    US Air Force, Res Lab, Combust Dynam Grp, 10 E Saturn Blvd,Bldg 8451, Edwards AFB, CA 93524 USA;

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