用格林函数方法分析热声模的相互作用

IF 1.4 4区 工程技术 Q3 ENGINEERING, MECHANICAL
A. Bigongiari, M. Heckl
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引用次数: 3

摘要

在本文中,我们将提出一种基于一维格林函数方法的快速预测工具,该工具可用于绕过数值昂贵的计算流体动力学模拟。格林函数方法的优点是提供了燃烧不稳定性产生和演变背后的物理学的清晰画面。此外,该方法允许我们进行模态分析;可以孤立地或与其他模式组合地处理单个声学模式。在这篇文章中,我们将研究高阶模态在决定系统稳定性中的作用。我们将首先分别生成第一和第二模式的稳定性图。然后将计算扰动的时间历程,其中两种模式都存在。火焰将通过通用火焰描述函数建模,即通过振幅相关火焰传递函数建模。时间历程计算显示了由初始扰动引起的两种模式的演变;揭示了瞬态振荡和极限循环振荡。我们的研究为燃烧过程中的非线性和非正态性建模迈出了第一步。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Analysis of the interaction of thermoacoustic modes with a Green’s function approach
In this paper, we will present a fast prediction tool based on a one-dimensional Green's function approach that can be used to bypass numerically expensive computational fluid dynamics simulations. The Green’s function approach has the advantage of providing a clear picture of the physics behind the generation and evolution of combustion instabilities. In addition, the method allows us to perform a modal analysis; single acoustic modes can be treated in isolation or in combination with other modes. In this article, we will investigate the role of higher-order modes in determining the stability of the system. We will initially produce the stability maps for the first and second mode separately. Then the time history of the perturbation will be computed, where both the modes are present. The flame will be modelled by a generic Flame Describing Function, i.e. by an amplitude-dependent Flame Transfer Function. The time-history calculations show the evolution of the two modes resulting from an initial perturbation; both transient and limit-cycle oscillations are revealed. Our study represents a first step towards the modelling of nonlinearity and non-normality in combustion processes.
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来源期刊
International Journal of Spray and Combustion Dynamics
International Journal of Spray and Combustion Dynamics THERMODYNAMICS-ENGINEERING, MECHANICAL
CiteScore
2.20
自引率
12.50%
发文量
21
审稿时长
>12 weeks
期刊介绍: International Journal of Spray and Combustion Dynamics is a peer-reviewed open access journal on fundamental and applied research in combustion and spray dynamics. Fundamental topics include advances in understanding unsteady combustion, combustion instability and noise, flame-acoustic interaction and its active and passive control, duct acoustics...
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