...
首页> 外文期刊>Combustion and Flame >Intrinsic flame instabilities in combustors: Analytic description of a 1-D resonator model
【24h】

Intrinsic flame instabilities in combustors: Analytic description of a 1-D resonator model

机译:燃烧室内的固有火焰不稳定性:一维共振器模型的解析描述

获取原文
获取原文并翻译 | 示例
           

摘要

The study is concerned with theoretical examination of thermo-acoustic instabilities in combustors and focuses on recently discovered 'flame intrinsic modes'. These modes differ qualitatively from the acoustic modes in a combustor. Although these flame intrinsic modes were intensely studied, primarily numerically and experimentally, the instability properties and dependence on the characteristics of the combustor remain poorly understood. Here we investigate analytically the properties of intrinsic modes within the framework of a linearized model of a quarter wave resonator with temperature and cross-section jump across the flame, and a linear n - tau model of heat release. The analysis of dispersion relation for the eigen-modes of the resonator shows that there are always infinite numbers of intrinsic modes present. In the limit of small interaction index n the frequencies of these modes depend neither on the properties of the resonator, nor on the position of the flame. For small n these modes are strongly damped. The intrinsic modes can become unstable only if n exceeds a certain threshold. Remarkably, on the neutral curve the intrinsic modes become completely decoupled from the environment. Their exact dispersion relation links the intrinsic mode eigen-frequency omega' with the mode number m' and the time lag tau: omega(1)= (2m' + 1)(7 pi/tau) + m pi/tau, where m = 0, +/-1. The main results of the study follow from the mode decoupling on the neutral curve and include explicit analytic expressions for the exact neutral curve on the n - tau plane, and the growth/decay rate dependence on the parameters of the combustor in the vicinity the neutral curve. The instability domain in the parameter space was found to have a very complicated shape, with many small islands of instability, which makes it difficult, if not impossible, to map it thoroughly numerically. The analytical results have been verified by numerical examination. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:该研究与燃烧器中热声不稳定性的理论研究有关,并且侧重于最近发现的“火焰固有模式”。这些模式在质量上与燃烧室中的声学模式不同。尽管对这些火焰的固有模式进行了深入的研究,主要是在数值和实验上,但对于燃烧器的不稳定性和对燃烧器特性的依赖性仍然知之甚少。在这里,我们在四分之一波谐振器的线性化模型(具有跨火焰的温度和横截面跃变)以及热释放的线性n-tau模型的框架内,对固有模式的性质进行了分析研究。对谐振器本征模的色散关系的分析表明,总是存在无限数量的本征模。在小的相互作用指数n的限制下,这些模式的频率既不取决于谐振器的特性,也不取决于火焰的位置。对于小n,这些模式被强烈阻尼。仅当n超过特定阈值时,本征模式才会变得不稳定。值得注意的是,在中性曲线上,固有模式变得与环境完全分离。它们的精确色散关系将固有模式本征频率omega'与模式编号m'和时滞tau链接在一起:omega(1)=(2m'+ 1)(7 pi / tau)+ m pi / tau,其中m = 0,+ /-1。该研究的主要结果来自中性曲线上的模态解耦,包括对n-tau平面上精确中性曲线的显式解析表达式,以及增长率/衰减率取决于中性点附近燃烧室的参数。曲线。发现参数空间中的不稳定性域具有非常复杂的形状,带有许多小的不稳定性岛,这使得即使不是不可能,也很难对其进行完整的数字映射。分析结果已通过数值检验得到验证。 (C)2017燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号