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Numerical Investigation of the Parameter Governing the Iqnitabilitv of a Sprav Flame

机译:Sprav火焰Iqnitabilitv控制参数的数值研究

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摘要

This paper contains a numerical examination concerning the ignition behavior of a spray nozzle mounted in a rectangular channel under atmospheric conditions, which is run with Jet A-I. On the basis of a comprehensive data set of experimental results, the numerical approach is verified primarily by means of a comparison of the flame growth and position after ignition. In the following, several distinct igniter positions and boundary condition settings are simulated. The conditions that prevail at the location of the ignition are investigated with respect to how they influence the ignition process. Due to changes in the fuel placement and flow field characteristics, which follow from alternating the boundary conditions, such as air and fuel mass flow, ignition is either promoted or impeded. The underlying causes that can lead to a success or failure of the ignition are analyzed. The ignition in the experiment is achieved through a laser-induced breakdown, which is modeled through a turbulent flame speed closure combustion model with an additional spark ignition extension. A comparison with the ignition statistics from the experiment shows that numerical tools can be used to determine preferential boundary conditions and igniter locations to accomplish a successful ignition in multiphase flow configurations.
机译:本文包含有关在大气条件下安装在矩形通道中的喷嘴的点火行为的数值研究,该喷嘴使用Jet A-I运行。在综合实验结果数据的基础上,主要通过比较火焰生长和点火后位置来验证数值方法。下面,模拟了几个不同的点火器位置和边界条件设置。关于它们如何影响点火过程,研究了在点火位置普遍存在的条件。由于交替改变边界条件(例如空气和燃料质量流量)而导致的燃料放置和流场特性发生变化,因此会促进或阻碍点火。分析了可能导致点火成功或失败的根本原因。实验中的点火是通过激光引起的击穿来实现的,该击穿是通过湍流火焰速度闭合燃烧模型和附加的火花点火扩展来模拟的。与来自实验的点火统计数据的比较表明,可以使用数值工具确定优先边界条件和点火器位置,以在多相流配置中成功完成点火。

著录项

  • 来源
    《Journal of Engineering for Gas Turbines and Power 》 |2013年第1期| 011506.1-011506.9| 共9页
  • 作者单位

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

    German Aerospace Center (DLR), Institute of Combustion Technology, Pfaffenwaldring 38-40, 70569 Stuttgart, Germany;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    flame propagation; ignition; multiphase flows; turbulent flame speed closure; droplet evaporation; lagrangian spray simulation;

    机译:火焰传播点火;多相流湍流火焰速度关闭;液滴蒸发拉格朗日喷雾模拟;

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