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Partially premixed reacting acetone spray using LES and FGM tabulated chemistry

机译:使用LES和FGM列表化学的部分预混合反应丙酮喷雾

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摘要

Large Eddy Simulations of dilute spray-air reacting two phase flow are performed following an Eulerian-Lagrangian approach. The method includes a full two-way coupling in which phase properties and spray source terms are interchanging between the two phases within each coupling time step. To achieve sub-grid scale closures in the filtered equations used for LES of the carrier phase, the Smagorinsky model with dynamic procedure is applied for the flow field while an eddy diffusivity approach is used for the scalar fluxes. The phase transition of droplets is captured using a non-equilibrium evaporation model. The evaporating droplets are tracked using a Langragian procedure. They are injected in a polydisperse manner and generated in time dependent boundary conditions. The combustion is described by a reaction progress variable and a mixture fraction as well as their variances in the line of the Flamelet Generated Manifold method. The ultimate objective of this work is to appraise the ability of this LES-based spray module developed here to retrieve the spray flow and combustion properties of the configuration under study. The configuration consists of a spray jet issued into a pilot flame and a co-flowing atmospheric air in which droplets traverse a pre-evaporation distance and release part of their mass before reaching the combustion zone. Thereby the spray pre-evaporation turns the combustion regime from diffusion to partially premixed. The fuel used is liquid acetone, which is modeled by a detailed reaction mechanism including 84 species and 409 elementary reactions. A series of spray established at different operating conditions are investigated, analyzed and compared. Analysis allows to gain a deep insight into the process ongoing. Comparisons include exhaust gas temperature, droplet velocities and corresponding fluctuations, droplet mean diameters and spray volume flux at different distances from the exit planes. An overall good agreement is reported.
机译:遵循欧拉-拉格朗日方法,对两相流中稀薄的喷雾空气进行反应的大涡模拟。该方法包括完全双向耦合,其中在每个耦合时间步长内,两相之间的相特性和喷雾源项相互交换。为了在用于载波相位的LES的滤波方程中实现亚网格规模的封闭,将具有动态过程的Smagorinsky模型应用于流场,而将涡流扩散率方法用于标量通量。使用非平衡蒸发模型捕获液滴的相变。使用Langragian程序跟踪蒸发的液滴。它们以多分散的方式注入,并在与时间相关的边界条件下生成。燃烧通过反应进度变量和混合物分数以及它们在“火焰产生歧管”方法行中的变化来描述。这项工作的最终目的是评估此处开发的基于LES的喷雾模块恢复所研究配置的喷雾流量和燃烧特性的能力。该配置包括喷入引燃火焰的喷射流和同流的大气,其中小滴穿过预蒸发距离并在到达燃烧区之前释放部分质量。由此,喷雾预蒸发使燃烧状态从扩散转变为部分预混合。所使用的燃料为液态丙酮,其通过详细的反应机理建模,包括84种和409个基本反应。研究,分析和比较了在不同操作条件下建立的一系列喷雾。通过分析,可以深入了解正在进行的过程。比较包括排气温度,液滴速度和相应的波动,液滴平均直径和与出口平面不同距离处的喷雾体积通量。据报告总体良好协议。

著录项

  • 来源
    《Combustion and Flame》 |2012年第8期|p.2718-2741|共24页
  • 作者单位

    Institute for Energy and Power Plant Technology, Department of Mechanical Engineering, TV Darmstadt, Petersenstr. 30, 64287 Darmstadt, Germany;

    School of Aerospace, Mechanical and Mechatronk Engineering, The University of Sydney, NSW 2006, Australia;

    Institute for Energy and Power Plant Technology, Department of Mechanical Engineering, TV Darmstadt, Petersenstr. 30, 64287 Darmstadt, Germany;

    School of Aerospace, Mechanical and Mechatronk Engineering, The University of Sydney, NSW 2006, Australia;

    Institute for Energy and Power Plant Technology, Department of Mechanical Engineering, TV Darmstadt, Petersenstr. 30, 64287 Darmstadt, Germany;

  • 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

    LES; partially premixed combustion; spray; FGM; euler-lagrange;

    机译:LES;部分预混燃烧;喷雾;女性生殖器;欧拉-拉格朗日;
  • 入库时间 2022-08-18 00:12:04

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