首页> 外文OA文献 >Modelin combustion of multicomponent fuel droplets: formulation and application to transportation fuels
【2h】

Modelin combustion of multicomponent fuel droplets: formulation and application to transportation fuels

机译:模拟多组分燃料液滴的燃烧:配方及其在运输燃料中的应用

摘要

The quasi-steady, spherically symmetric combustion of multicomponent isolated fueldroplets has been modeled using modified Shvab-Zeldovich variable mechanism. Newlydeveloped modified Shvab-Zeldovich equations have been used to describe the gas phasereactions. Vapor-liquid equilibrium model has been applied to describe the phase change at thedroplet surface. Constant gas phase specific heats are assumed. The liquid phase is assumed tobe of uniform composition and temperature. Radiative heat transfer between the droplet andsurroundings is neglected.The results of evaporation of gasoline with discrete composition of hydrocarbons have beenpresented. The evaporation rates seem to follow the pattern of volatility differentials. Theevaporation rate constant was obtained as 0.344mm2/sec which compared well with the unsteadyresults of Reitz et al. The total evaporation time of the droplet at an ambience of 1000K wasestimated to be around 0.63 seconds. Next, the results of evaporation of representative dieselfuels have been compared with previously reported experimental data. The previous experimentsshowed sufficient liquid phase diffusional resistance in the droplet. Numerical results areconsistent with the qualitative behavior of the experiments. The quantitative deviation during thevaporization process can be attributed to the diffusion time inside the droplet which isunaccounted for in the model. Transient evaporation results have also been presented for therepresentative diesel droplets. The droplet temperature profile indicates that the droplettemperature does not reach an instantaneous steady state as in the case of single-componentevaporation.To perform similar combustion calculations for multicomponent fuel droplets, no simplemodel existed prior to this work. Accordingly, a new simplified approximate mechanism formulticomponent combustion of fuel droplets has been developed and validated against severalindependent data sets. The new mechanism is simple enough to be used for computationalstudies of multicomponent droplets.The new modified Shvab-Zeldovich mechanism for multicomponent droplet combustion hasbeen used to model the combustion characteristics of a binary alcohol-alkane droplet andvalidated against experimental data. Burn rate for the binary droplet of octanol-undecane wasestimated to be 1.17mm2/sec in good concurrence with the experimental value of 0.952mm2/secobtained by Law and Law. The model has then been used to evaluate the combustioncharacteristics of diesel fuels assuming only gas phase reactions. Flame sheet approximation hasbeen invoked in the formulation of the model.
机译:使用改进的Shvab-Zeldovich可变机制对多组分隔离燃料滴的准稳态,球对称燃烧进行了建模。新开发的改进的Shvab-Zeldovich方程已用于描述气相反应。汽液平衡模型已被用来描述液滴表面的相变。假定恒定的气相比热。假定液相具有均匀的组成和温度。忽略了液滴与周围环境之间的辐射传热。提出了具有离散碳氢化合物组成的汽油的蒸发结果。蒸发速率似乎遵循波动率差异的模式。蒸发速率常数为0.344mm2 / sec,与Reitz等人的不稳定结果相比较。在1000K的环境下,液滴的总蒸发时间估计为约0.63秒。接下来,将代表性柴油的蒸发结果与先前报道的实验数据进行了比较。先前的实验表明液滴中有足够的液相扩散阻力。数值结果与实验的定性行为一致。汽化过程中的定量偏差可以归因于液滴内部的扩散时间,而该扩散时间在模型中未说明。还已经给出了代表性柴油滴的瞬态蒸发结果。液滴温度曲线表明,液滴温度没有达到单组分蒸发情况下的瞬时稳态。要对多组分燃料液滴进行相似的燃烧计算,在此工作之前没有简单的模型。因此,已经开发了一种新的简化的用于燃料小滴多组分燃烧的近似机制,并针对几个独立的数据集进行了验证。这种新的机制很简单,可以用于多组分液滴的计算研究。新的改进的Shvab-Zeldovich多组分液滴燃烧机理用于模拟二元醇-烷烃液滴的燃烧特性,并根据实验数据进行了验证。良好的一致性估计辛醇-十一烷的二元液滴的燃烧速率为1.17mm2 / sec,Law and Law获得的实验值为0.952mm2 / sec。然后,仅假设气相反应,该模型已用于评估柴油的燃烧特性。在模型的制定中已经调用了火焰表近似法。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号