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Numerical investigation of the flow and flame structure in an axisymmetric trapped vortex combustor

机译:轴对称截留涡流燃烧器内流动和火焰结构的数值研究

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摘要

The main intention of the present investigation is to bring out the effect of the momentum flux ratio (MFR) on the flow and flame structure in an axisymmetric Trapped Vortex Combustor (TVC). In this study, the MFR was varied by changing the secondary air jet velocity, while keeping the fuel, primary and the mainstream air velocities constant. This study revealed that a single vortex, embedded within a flame on its edge was formed in the cavity for the low MFR case (MFR ~ 0.57) for which intense burning was observed at the shear layer. In contrast, for the higher MFR cases {MFR ~ 0.82 and 1.8), the flow and flame structures were altered considerably due to the occurrence of multiple vortices within the cavity. A comparison with the previous cold flow study revealed that the change in flow structure was attributed to the volume expansion due to the heat release during the combustion. Besides this, a counter rotating primary vortex was formed near the bottom wall, which grew in size with the MFR. As a result, the shape of the cavity flame was altered, which may protrude out of the cavity, leading to the local quenching of the flame. Hence, it could be concluded that the momentum flux ratio plays an important role in altering the flow and flame structures within the TVC cavity, thus affecting the performance of the combustor.
机译:本研究的主要目的是揭示动量通量比(MFR)对轴对称捕集式涡流燃烧器(TVC)中的流动和火焰结构的影响。在这项研究中,通过改变次级空气喷射速度来改变MFR,同时保持燃料,初级和主流空气速度不变。这项研究表明,对于低MFR情况(MFR〜0.57),在剪切层观察到强烈燃烧,在空腔中形成了一个嵌入涡流的火焰。相反,对于较高的MFR情况(MFR〜0.82和1.8),由于在腔体内出现多个涡流,流动和火焰结构发生了很大变化。与先前冷流研究的比较表明,流动结构的变化归因于燃烧过程中放热引起的体积膨胀。除此之外,在底壁附近形成了反向旋转的初级涡流,该涡旋随着MFR的增大而增大。结果,空腔火焰的形状发生了变化,可能会从空腔中伸出,导致火焰局部熄灭。因此,可以得出结论,动量通量比在改变TVC腔内的流动和火焰结构中起着重要作用,从而影响燃烧室的性能。

著录项

  • 来源
    《Fuel》 |2012年第2012期|p.78-84|共7页
  • 作者

    P.K. Ezhil Kumar; D.P. Mishra;

  • 作者单位

    Combustion Lab, Department of Aerospace Engineering, Indian Institute of Technology, Kanpur 208 016, India;

    Combustion Lab, Department of Aerospace Engineering, Indian Institute of Technology, Kanpur 208 016, India;

  • 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

    trapped vortex; gas turbine combustor; momentum flux ratio; flame structure;

    机译:涡旋燃气轮机燃烧器动量通量比火焰结构;

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