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Modelling two-phase flow and transport effects of multi-component fuels

机译:模拟多组分燃料的两相流和输运效果

摘要

Three novel multicomponent fuel spray droplet evaporation models are developed by employing the theory of continuous thermodynamics(CT) with the aim of applying them in the design and analysis of various energy conversion devices such as, aircraft jet engines, liquid-fuel rocket engines, diesel engines, and industrialfurnaces. The CT methodology seeks to represent complex mixtures - for example,aviation kerosene or JP8 that typically comprise blends of a large number of chemical compounds by using probability distribution functions (PDFs). The components of JP8, which is constituted by the homologous series of paraffin, naphthene, and aromatic hydrocarbons; are each represented by the Pearson-Shultz type three-parameter gamma PDF, where the three (shape, scale, and origin) parameters characterise changes in the mixture composition. The phase transition of the liquid droplet due to evaporation is modelled using both low-pressure (LP) and high-pressure (HP) vapour-liquid equilibrium (VLE) models employing various mixing and combining rules by applying a general cubic equation of state (CEOS). Interestingly enough, the phase transition of the liquid fuel into vapour mixture is characterised by a change in the PDF scale parameter alone. Once the description of the fuel mixture is complete, the traditional species and energy transport equationsboth for the liquid and vapour phases respectively, are re-written using the composition PDF moments underLagrangian and Eulerian frameworks. In order to solve the governing equations for the three droplet evaporation models, which characteristically involve phase change and a moving interface, a novel fullyAdaptive Method Of Lines using B-Spline Collocation (AMOLBSC) is developed. The models are tested at various pressures, temperatures and convective conditions, including at a lean, premixed, prevaporised (LPP) combustor operating condition. In general, the computational results at an ambient pressure close to atmospheric showed good to excellent agreement against available experimental data in the literature.However, for ambient conditions with elevated-high pressures and temperatures only models that employ the HP formulation gave reliable results. In particular, when the liquid is at or near its critical pressure and temperature it is characterised by faster vaporisation and shorter droplet lifetime, including some evidence ofliquid mass diffusion. The liquid model that incorporates the effects of liquid core circulation using semiempiricalapproximation and adaptive mesh refinement (AMR) technique is the most accurate andcomputationally efficient, although further work is required to establish its ranges of applicability.
机译:运用连续热力学(CT)理论开发了三种新颖的多组分燃油喷雾蒸发模型,旨在将其应用于飞机,喷气发动机,液体燃料火箭发动机,柴油机等各种能量转换装置的设计和分析中发动机和工业炉。 CT方法学试图通过概率分布函数(PDF)来表示复杂的混合物,例如航空煤油或JP8,这些混合物通常包含大量化学化合物的混合物。 JP8的成分,由石蜡,环烷烃和芳烃的同源系列组成;分别由Pearson-Shultz类型的三参数gamma PDF表示,其中三个(形状,比例和原点)参数表征混合物成分的变化。使用低压(LP)和高压(HP)汽-液平衡(VLE)模型对由于蒸发而产生的液滴的相变进行建模,该模型采用各种混合和组合规则,通过应用一般的状态立方方程( CEOS)。有趣的是,液体燃料向蒸气混合物的相变仅通过PDF标度参数的变化来表征。一旦完成了对燃料混合物的描述,就分别在Lagrangian和Eulerian框架下使用PDF矩组成重写了分别针对液相和气相的传统物质和能量传输方程式。为了解决三个液滴蒸发模型的控制方程,这些模型典型地涉及相变和运动界面,开发了一种新颖的使用B样条搭配的完全自适应线法(AMOLBSC)。该模型在各种压力,温度和对流条件下进行了测试,包括在稀薄,预混合,预蒸发(LPP)燃烧室的运行条件下。通常,在接近大气压的环境压力下的计算结果与文献中的可用实验数据显示出极好的一致性,但是,对于高压和高温环境条件,只有采用HP配方的模型才能给出可靠的结果。特别地,当液体处于或接近其临界压力和温度时,其特征在于更快的汽化和更短的液滴寿命,包括一些液体质量扩散的证据。尽管需要进一步的工作来确定其适用范围,但使用半经验近似和自适应网格细化(AMR)技术结合液芯循环影响的液体模型是最准确且计算效率最高的模型。

著录项

  • 作者

    Maru Wessenu-Abegaz;

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  • 年度 2005
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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