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Elucidating the Properties of Surrogate Fuel Mixtures Using Molecular Dynamics

机译:使用分子动力学阐明替代燃料混合物的性质

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The wide compositional differences between conventional and alternative fuels have resulted in much research aimed at determining which alternative fuels can be used, and in what proportions, in conventional engines. Atomic-scale modeling is uniquely positioned to lend insight into this question without extensive large-scale tests. The predictive power such modeling affords could narrow the phase space that must be examined experimentally. This study utilizes molecular dynamics (MD) simulations to predict the properties of a set of pure hydrocarbons, as well as binary and multicomponent surrogate fuel mixtures for alternative fuels created from these pure components. The accuracy and transferability of the modified Lennard-Jones adaptive intermolecular reactive empirical bond-order potential (mod-LJ AIREBO) [Liu, A.; Stuart, S. J. J. Comput. Chem. 2008, 29, 601-611] was assessed by calculating densities, heats of vaporization, and bulk moduli of pure hydrocarbons and the mixtures of these hydrocarbons, i.e., surrogate fuels. Calculated results were compared to experimentally determined values and to values obtained with the nonreactive, all-atom version of the optimized potential for liquid simulations (OPLS-AA) [Jorgensen, W. L.; Maxwell, D. S.; TiradoRives, J. J. Am. Chem. Soc. 1996, 118, 11225-11236]. The mod-LJ AIREBO potential quantitatively predicts the densities of the pure hydrocarbons and binary mixtures of n-dodecane and 2,2,4,4,6,8,8-heptamethylnonane (isocetane). It is interesting to note, that despite doing an excellent job predicting the densities of the pure hydrocarbons, the performance of the mod-LJ AIREBO potential degrades when predicting the densities of the multicomponent surrogates and mixtures of n-hexadecane and isocetane, implying that it is not straightforward to extend potentials fit with pure compounds to mixtures. The OPLS-AA potential also has difficulty quantitatively predicting the densities of mixtures, although a new parameter set for long-chain hydrocarbons (L-OPLS) [Siu, S. W. I.; Pluhackova, K.; Bockmann, R. A. J. Chem. Theory Comput. 2012, 8, 1459-1470] yields some improvement for binary mixtures. Heat of vaporization predictions using both potentials also agree reasonably well with experiment. Bulk moduli predictions using the mod-LJ AIREBO potential are consistently higher than, and do not quantitatively agree with, the experimental values. In contrast, bulk moduli predictions using the OPLS-AA potential are generally in good agreement with experimental values. Despite the success of the OPLS-AA potential predicting the bulk moduli of individual hydrocarbons, it is unable to quantitatively predict the bulk moduli of the multicomponent surrogates. Interestingly, the use of the L-OPLS parameter set improves density predictions but not predicted bulk moduli values.
机译:常规燃料和替代燃料之间的巨大成分差异导致了许多研究,旨在确定常规发动机中可以使用哪种替代燃料以及以何种比例使用。原子级建模的独特位置在于无需进行大规模的大规模测试即可深入了解该问题。这种建模提供的预测能力可以缩小必须通过实验检查的相空间。这项研究利用分子动力学(MD)模拟来预测一组纯烃的性质,以及由这些纯组分产生的替代燃料的二元和多组分替代燃料混合物。改良的Lennard-Jones自适应分子间反应性经验键序势(mod-LJ AIREBO)的准确性和可传递性[Liu,A .; Stuart,S。J. J. Comput。化学[2008,29,601-611]通过计算密度,汽化热和纯碳氢化合物以及这些碳氢化合物(即替代燃料)混合物的体积模量进行评估。将计算结果与实验确定的值以及使用非反应性全原子版本的液体模拟优化电位(OPLS-AA)所获得的值进行比较(Jorgensen,W. L .;麦克斯韦(美国)。 TiradoRives,J。J. Am。化学Soc。 1996,118,11225-11236]。 mod-LJ AIREBO电势可定量预测正十二烷和2,2,4,4,6,8,8-庚甲基壬烷(异十六烷)的纯烃和二元混合物的密度。有趣的是,尽管在预测纯烃的密度方面做得很出色,但在预测正十六烷和异十六烷的多组分替代物和混合物的密度时,mod-LJ AIREBO电势的性能却下降了,这意味着将简单化合物的潜力扩展到混合物并非易事。尽管对于长链烃(L-OPLS)设置了新的参数,但OPLS-AA的潜力也难以定量地预测混合物的密度[Siu,S.W.I。; S.W.I.; S.W.I。]。 K.Pluhackova; Bockmann,R.A.J.Chem。理论计算。 [2012,8,1459-1470]对二元混合物产生了一些改进。使用这两个电位的汽化热预测值也与实验相当吻合。使用mod-LJ AIREBO电势的体积模量预测值始终高于实验值,并且在数量上与实验值不一致。相反,使用OPLS-AA势的体积模量预测通常与实验值非常吻合。尽管OPLS-AA潜力成功地预测了单个烃的体积模量,但它无法定量预测多组分替代物的体积模量。有趣的是,使用L-OPLS参数集可以提高密度预测,但不能提高体积模量预测值。

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  • 来源
    《Energy & fuels》 |2016年第2期|784-795|共12页
  • 作者单位

    US Naval Acad, Dept Chem, Annapolis, MD 21402 USA;

    US Naval Acad, Dept Chem, Annapolis, MD 21402 USA;

    Rochester Inst Technol, Sch Phys & Astron, Rochester, NY 14623 USA;

    US Naval Acad, Dept Chem, Annapolis, MD 21402 USA;

    US Naval Acad, Dept Chem, Annapolis, MD 21402 USA;

    US Naval Res Lab, Div Chem, Washington, DC 20375 USA;

    Oakland Univ, Dept Mech Engn, Rochester, MI 48309 USA;

    US Naval Acad, Dept Chem, Annapolis, MD 21402 USA;

    High Point Univ, Dept Chem, High Point, NC 27262 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
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  • 入库时间 2022-08-18 00:39:54

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