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Experimental and computational study on partially premixed flames in a centerbody burner

机译:中心燃烧器中部分预混火焰的实验和计算研究

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摘要

The centerbody burner was designed with the objective of understanding the coupled processes of soot formation, growth, and burnout. Fuel that issues from the center of the burner establishes two flame zones - one associated with the recirculation zone (RZ) and the other, with the trailing jet. The sooting characteristics in these two flame zones can be quite different because of variations in residence time and transport of reactants and products. Calculations performed for this burner operating under a partially premixed fuel jet suggested that soot in the RZ decreases and that soot in the trailing jet flame increases with the amount of premixing. An experimental and numerical study is performed to aid the understanding of these differences. A time-dependent, axisymmetric, detailed-chemistry computa-tional-fluid-dynamics (CFD) model known as Unsteady Ignition and Combustion using ReactioNs (UNICORN) is used for simulating flames under different equivalence-ratio conditions. Combustion and PAH formation are modeled using the Wang-Frenklach (99 species and 1066 reactions) mechanism, and soot is simulated using a two-equation model of Lindstedt. A Lagrangian-based particle-tracking model is used for understanding the evolution of soot-like particles. Flame and recirculation-zone structures and soot in the experiments are identified using direct photographs taken with and without Mie scattering from soot particles as well as laser-induced-incandescence (LII) measurements. Calculations predict the structures of the partially premixed centerbody flames for various equivalence ratios reasonably well. Experiments confirm the predicted soot suppression in the RZs and enhancement of soot in the trailing jet flame when air is added to the fuel jet. It is found that flame movement in the RZ increases soot-particle burnout and, thereby, reduces the amount of soot within the RZ. As the flame moves closer to the fuel jet, more soot becomes entrained into the inner vortex. Motion of soot-like particles explained the spiral rings observed in the experiment. Increased particle burnout with partial premixing leads to shrinkage of soot spirals.
机译:中心燃烧器的设计目的是了解烟灰形成,生长和燃尽的耦合过程。从燃烧器中心发出的燃料建立了两个火焰区-一个与再循环区(RZ)相关联,另一个与尾随射流相连。由于停留时间以及反应物和产物的传输的变化,这两个火焰区的烟ot特性可能会完全不同。对于在部分预混燃料射流下运行的燃烧器进行的计算表明,随着预混量的增加,RZ中的煤烟减少,尾随火焰中的煤烟增加。进行了实验和数值研究以帮助理解这些差异。使用时间依赖性,轴对称,详细化学计算流体动力学(CFD)模型(使用ReactioNs进行非稳态点火和燃烧)(UNICORN)来模拟不同当量比条件下的火焰。使用Wang-Frenklach(99种和1066个反应)机理对燃烧和PAH的形成进行建模,并使用Lindstedt的两方程模型对烟灰进行模拟。基于拉格朗日的粒子跟踪模型用于理解烟灰状粒子的演化。实验中的火焰和再循环区结构以及烟灰是使用直接照片拍摄的,该照片带有或不带有烟灰颗粒的Mie散射以及激光诱导的白炽度(LII)测量。通过计算,可以很好地预测部分当量混合比的中心体火焰的结构。实验证实了当将空气添加到燃料喷嘴中时,预测的RZs中的烟灰抑制作用和尾随火焰中烟灰的增强作用。发现RZ中的火焰运动增加了烟灰颗粒的燃尽,从而减少了RZ内的烟灰量。随着火焰移近燃料喷嘴,更多的烟灰被夹带到内部涡流中。烟灰状颗粒的运动解释了实验中观察到的螺旋环。部分预混会增加颗粒燃尽,导致烟灰螺旋收缩。

著录项

  • 来源
    《Combustion and Flame》 |2011年第3期|p.511-524|共14页
  • 作者单位

    Innovative Scientific Solutions Inc., 2766 Indian Ripple Road, Dayton, OH 45440, United States;

    Innovative Scientific Solutions Inc., 2766 Indian Ripple Road, Dayton, OH 45440, United States;

    Propulsion Directorate, Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, United States;

    Propulsion Directorate, Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, United States;

    Propulsion Directorate, Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, United States;

    Propulsion Directorate, Air Force Research Laboratory, Wright-Patterson Air Force Base, OH 45433, United States;

    University of Dayton Research Institute, 300 College Park Dayton, OH 45469, United States;

    Spectral Energies, LLC, 5100 Springfield Street, Dayton, OH 45431, United States;

  • 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

    partially premixed flames; soot; laminar flames; modeling;

    机译:部分预混火焰;煤烟;层流火焰造型;
  • 入库时间 2022-08-18 00:12:15

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