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Effect of vorticity waves on azimuthal instabilities in annular chambers

机译:涡度波对环形室方位角不稳定性的影响

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摘要

Azimuthal instabilities are the thermoacoustic oscillations that appear in the annular chambers of gas turbines. In previous investigations, the voracity waves that can be generated by the interaction of acoustic waves and flame have typically been neglected. The Present paper studies how vorticity waves affect the azimuthal instability in a simple annular chamber with a compacted flame sheet. An analytical model with the effect of the vorticity wave is constructed. To validate this analytical model with the voracity wave, a linear Euler equation method, in which all forms of flow disturbances are included, is introduced. The results from the analytical method without the voracity wave are also given, on the analogy of the network model and finite element method. Good agreement is found between the numerical simulation on the basis of the linear Euler equation and the analytical method with voracity disturbance. Moreover, for the pure azimuthal mode, the difference between the results with and without voracity disturbance is significant. For axial and azimuthal mixed-mode, the effect of voracity disturbance is weak. These results show that the calculation of azimuthal instabilities using a network model and finite element method may lead to severe prediction errors when the mean flow is considered. The generation of vorticity disturbance is also studied based on both numerical method and dimensional analysis. It is concluded that in the present case, the generation of vorticity disturbance is due to the circumferential velocity continuity across the flame. (C) 2014 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:方位角不稳定性是出现在燃气轮机环形室中的热声振荡。在以前的研究中,通常会忽略由声波和火焰相互作用产生的挥发性波。本文研究了涡流波如何影响带有密实火焰片的简单环形腔室中的方位角不稳定性。建立了具有涡度波影响的解析模型。为了用流动性波验证该分析模型,引入了线性欧拉方程法,其中包括了所有形式的流动扰动。类似于网络模型和有限元方法,还给出了没有波动率波的分析方法的结果。在线性欧拉方程基础上的数值模拟与带有扰动的解析方法之间找到了很好的一致性。此外,对于纯方位角模式,在有和没有扰动的情况下,结果之间的差异是很大的。对于轴向和方位混合模式,孔隙度扰动的影响较弱。这些结果表明,当考虑平均流量时,使用网络模型和有限元方法计算方位不稳定性可能会导致严重的预测误差。还基于数值方法和尺寸分析研究了涡旋扰动的产生。可以得出结论,在当前情况下,涡旋扰动的产生是由于整个火焰的圆周速度连续性造成的。 (C)2014年燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

  • 来源
    《Combustion and Flame》 |2015年第3期|628-641|共14页
  • 作者

    Li Lei; Sun Xiaofeng;

  • 作者单位

    Beijing Univ Aeronaut & Astronaut, Sch Jet Prop, Beijing 100191, Peoples R China;

    Beijing Univ Aeronaut & Astronaut, Sch Jet Prop, Beijing 100191, Peoples R China;

  • 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

    Azimuthal instability; Combustion instability; Vorticity wave; Annular chamber;

    机译:方位不稳定性;燃烧不稳定性;涡度波;环形室;
  • 入库时间 2022-08-18 00:11:06

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