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Combustion kinetic modeling using multispecies time histories in shock-tube oxidation of heptane

机译:庚烷冲击管氧化中使用多种时间历史的燃烧动力学建模

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摘要

Recently, species time histories have been measured during n-heptane oxidation behind reflected shock waves [D.F. Davidson, Z. Hong, G.L. Pilla, A. Farooq, R.D. Cook, R.K. Hanson, Combust. Flame 157 (2010) 1899-1905]. The highly precise nature of these measurements is expected to impose critical constraints on chemical kinetic models of hydrocarbon combustion. In this paper, we apply the Method of Uncertainty Analysis using Polynomial Chaos Expansions (MUM-PCE) [D.A. Sheen, X. You, H. Wang, T. Lovas, Proc. Combust. Inst. 32 (2009) 535-542] to demonstrate how the multispecies measurement may be utilized beyond simple model validation. The results show that while an as-compiled, prior reaction model of n-alkane combustion can be accurate in its prediction of the detailed species profiles, the kinetic parameter uncertainty in the model remains to be too large to obtain a precise prediction of the data. Constraining the prior model against the species time histories within the measurement uncertainties led to notable improvements in the precision of model predictions against the species data as well as the global combustion properties considered. Lastly, we show that while the capability of the multispecies measurement presents a step-change in our precise knowledge of the chemical processes in hydrocarbon combustion, accurate data of global combustion properties are still necessary to predict fuel combustion.
机译:最近,在正庚烷氧化过程中,在反射冲击波之后测量了物种的时间历史[D.F. Davidson,Z.Hong,G.L. Pilla,A.Farooq,R.D. Cook,R.K.汉森,燃烧。火焰157(2010)1899-1905]。这些测量的高度精确性有望对碳氢化合物燃烧的化学动力学模型施加严格的限制。在本文中,我们应用了使用多项式混沌扩展(MUM-PCE)进行的不确定性分析方法[D.A. Sheen,X. You,H. Wang,T.Lovas,Proc。燃烧研究所32(2009)535-542]展示了如何在简单模型验证之外利用多物种测量。结果表明,尽管已编译的正构烷烃燃烧反应模型可以准确预测详细的物种分布,但模型中的动力学参数不确定性仍然太大,无法获得准确的数据预测。在测量不确定性内将先前模型限制在物种时间历史范围内,从而导致针对物种数据的模型预测精度以及所考虑的整体燃烧特性有了显着提高。最后,我们表明,尽管多物种测量的能力在我们对碳氢化合物燃烧化学过程的精确了解中呈现出阶跃式变化,但仍需要全球燃烧特性的准确数据来预测燃料燃烧。

著录项

  • 来源
    《Combustion and Flame》 |2011年第4期|p.645-656|共12页
  • 作者

    David A. Sheen; Hai Wang;

  • 作者单位

    Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, CA 90089, USA;

    Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, CA 90089, 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

    combustion kinetics; shock tube; modeling; uncertainty analysis;

    机译:燃烧动力学冲击管造型;不确定性分析;
  • 入库时间 2022-08-18 00:12:12

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