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Investigation of Blowoff Mechanism and Forced Response of Bluff Body Stabilized Turbulent Premixed Flames.

机译:钝体稳定湍流预混火焰的喷吹机理和强迫响应研究。

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摘要

Important problems related to the governing mechanism of flame blowoff in bluff body stabilized turbulent premixed combustion have been investigated in this dissertation. In the first part of the dissertation fundamental aspects of unforced and forced response in premixed and partially premixed fuel stratified flames encountered in low NOx gas turbine engines and afterburners are studied. Combustion in these devices presents complexities and instabilities introduced by thereto-acoustic, entropy wave and convective interactions. In this context, generalized blowoff limits and transfer functions of premixed turbulent flames under controlled acoustic perturbations and mixture gradients have been characterized.;The second part of the study concerns the flame dynamics of a bluff body stabilized turbulent premixed flame as it approaches lean blowoff. Experiments were performed in a laboratory scale burner as well as in a prototypical combustor with different geometries (axisymmetric and planar two dimensional), length and velocity scales. High speed chemiluminescence imaging along with simultaneous particle imaging velocimetry and OH planar laser-induced fluorescence were utilized in both these experiments for premixed propane-air flames to determine the sequence of events leading to blowoff and provide a quantitative analysis of the experimental data. It was found that near blowoff, the flame front and shear layer vortices overlap as a result of the reduced flame speed in fuel lean mixtures, to induce high local stretch rates on the flame. The high stretch rates exceeded the extinction stretch rate values instantaneously and in the mean, resulting in local flame extinction along the shear layers. Following partial or whole shear layer extinction, fresh reactants could pass through the non-reacting shear layers to react within the recirculation zone with some or all other parts of the flame extinguished. The flame kernel within the recirculation zone might survive for a few milliseconds and could reignite the shear layers such that the entire flame can be reestablished for a short period. This extinction and reignition event could happen several times before final blowoff event which occurred when the flame kernel failed to reignite the shear layers and ultimately lead to total flame extinguishment. Strikingly similar findings in the two different experimental setups suggest the general validity of the proposed flame blowoff mechanism and its insensitivity to a particular geometry.;Finally, recent results from ongoing research on the mechanism of forced blowoff and an experimental study on scalar mixing in an interacting field of two successively generated counter rotating laminar line vortices at the interface of two gas streams are presented.
机译:本文研究了钝体稳定湍流预混燃烧中火焰吹除控制机理的重要问题。在论文的第一部分中,研究了在低NOx燃气涡轮发动机和加力燃烧器中遇到的预混合和部分预混合燃料分层火焰中的非强制和强制响应的基本方面。这些装置中的燃烧呈现出由声,熵波和对流相互作用引起的复杂性和不稳定性。在这种情况下,已经表征了在受控声扰动和混合梯度下的预混湍流火焰的一般吹扫极限和传递函数。;研究的第二部分涉及钝态稳定的湍流预混火焰接近稀薄吹气时的火焰动力学。实验在实验室规模的燃烧器以及具有不同几何形状(轴对称和平面二维),长度和速度尺度的原型燃烧器中进行。在这两个实验中,均使用高速化学发光成像以及同时的粒子成像测速和OH平面激光诱导的荧光对丙烷-空气火焰进行预混,以确定导致爆燃的事件顺序,并对实验数据进行定量分析。已经发现,由于贫燃料混合物中火焰速度的降低,在接近喷出时,火焰前沿和剪切层涡旋重叠,从而在火焰上引起较高的局部拉伸率。高拉伸速率瞬间超过平均熄灭拉伸速率值,导致沿剪切层的局部火焰熄灭。在部分或全部剪切层消失之后,新鲜的反应物可以通过未反应的剪切层,以在再循环区内与火焰的一些或全部其他部分反应。再循环区内的火焰核可能存活数毫秒,并可能重新点燃剪切层,从而可以在短时间内重建整个火焰。这种熄灭和复燃事件可能在最终吹灭事件发生之前发生了好几次,最后一次吹灭事件是在火焰核未能重新点燃剪切层并最终导致火焰完全熄灭时发生的。在两个不同的实验装置中,惊人的相似发现表明拟议的火焰吹除机理具有普遍的有效性,并且对特定的几何形状不敏感。最后,正在进行的关于强制吹除机理的研究和标量混合在标量混合中的实验研究的最新结果给出了两个气流交界面处两个相继产生的反向旋转层流涡旋的相互作用场。

著录项

  • 作者

    Chaudhuri, Swetaprovo.;

  • 作者单位

    University of Connecticut.;

  • 授予单位 University of Connecticut.;
  • 学科 Applied Mechanics.;Engineering Mechanical.;Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 208 p.
  • 总页数 208
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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