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Large Eddy Simulation of High Reynolds Number Nonreacting and Reacting JP-8 Sprays in a Constant Pressure Flow Vessel With a Detailed Chemistry Approach

机译:采用详细化学方法在恒压流容器中对高雷诺数未反应和反应的JP-8喷雾进行大涡模拟

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摘要

In military propulsion applications, the characterization of internal combustion engines operating with jet fuel is vital to understand engine performance, combustion phasing, and emissions when JP-8 is fully substituted for diesel fuel. In this work, high-resolution large eddy simulation (LES) simulations have been performed in-order to provide a comprehensive analysis of the detailed mixture formation process in engine sprays for nozzle configurations of interest to the Army. The first phase examines the behavior of a non-reacting evaporating spray, and demonstrates the accuracy in predicting liquid and vapor transient penetration profiles using a multirealization statistical grid-converged approach. The study was conducted using a suite of single-orifice injectors ranging from 40 to 147 μm at a rail pressure of 1000 bar and chamber conditions at 900 K and 60 bar. The next phase models the nonpremixed combustion behavior of reacting sprays and investigates the submodel ability to predict auto-ignition and lift-off length (LOL) dynamics. The model is constructed using a Kelvin Helmholtz-Rayleigh Taylor (KH-RT) spray atomization framework coupled to an LES approach. The liquid physical properties are defined using a JP-8 mixture containing 80% n-decane and 20% trimethylbenzene (TMB), while the gas phase utilizes the Aachen kinetic mechanism (Hummer, et al., 2007, "Experimental and Kinetic Modeling Study of Combustion of JP-8, Its Surrogates, and Reference Components in Laminar Non Premixed Flows," Proc. Combust. Inst., 31, pp. 393-400 and Honnet, et al., 2009, "A Surrogate Fuel for Kerosene," Proc. Combust. Inst., 32, pp. 485-492) and a detailed chemistry combustion approach. The results are in good agreement with the spray combustion measurements from the Army Research Laboratory (ARL), constant pressure flow (CPF) facility, and provide a robust computational framework for further JP-8 studies of spray combustion.
机译:在军事推进应用中,使用喷气燃料运行的内燃机的特性对于理解JP-8完全替代柴油燃料时的发动机性能,燃烧定相和排放至关重要。在这项工作中,已进行了高分辨率大涡模拟(LES)模拟,以便对陆军感兴趣的喷嘴配置的发动机喷雾剂中详细的混合物形成过程提供全面的分析。第一阶段检查非反应性蒸发喷雾的行为,并演示使用多实现统计网格融合方法预测液体和蒸气瞬态渗透曲线的准确性。该研究是使用一套单孔喷射器进行的,该喷射器的喷射压力范围为40至147μm,轨道压力为1000 bar,腔室条件为900 K和60 bar。下一阶段对反应喷雾的非预混燃烧行为进行建模,并研究子模型预测自动点火和升程长度(LOL)动态的能力。该模型是使用结合LES方法的Kelvin Helmholtz-Rayleigh Taylor(KH-RT)喷雾雾化框架构建的。使用包含80%正癸烷和20%三甲基苯(TMB)的JP-8混合物定义液体物理性质,而气相利用Aachen动力学机理(Hummer等,2007,“实验和动力学模型研究”层流非预混流中JP-8的燃烧,其替代物和参考组分”,Proc.Combust.Inst。,第31卷,第393-400页,Honnet等人,2009年,“一种用于煤油的替代燃料, “ Proc。Combust。Inst。,32,第485-492页)和详细的化学燃烧方法。结果与陆军研究实验室(ARL),恒压流量(CPF)设施的喷雾燃烧测量结果非常吻合,并为进一步的JP-8喷雾燃烧研究提供了可靠的计算框架。

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  • 来源
    《Journal of Energy Resources Technology》 |2016年第3期|032207.1-032207.12|共12页
  • 作者单位

    U.S. Army Research Laboratory, 4603 Flare Loop Drive, Aberdeen Proving Ground, MD 21005;

    Convergent Science, Inc., 6400 Enterprise Ln, Madison, WI 53719;

    Convergent Science, Inc., 6400 Enterprise Ln, Madison, WI 53719;

    Convergent Science, Inc., 6400 Enterprise Ln, Madison, WI 53719;

    U.S. Army Research Laboratory, 4603 Flare Loop Drive, Aberdeen Proving Ground, MD 21005;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 00:28:07

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