Analytical Analysis of Indirect Combustion Noise in Subcritical Nozzles

A. Giauque, M. Huet, F. Cléro
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引用次数: 66

Abstract

This article revisits the problem of indirect combustion noise in nozzles of finite length. The analytical model proposed by Moase et al. (JFM 2007) for indirect combustion noise is red-erived and applied to subcritical nozzles having shapes of increasing complexity. This model is based on the equations formulated by Marble & Candel (JSV 1977) for which an explicit solution is obtained in the subsonic framework. The discretization of the nozzle into n elementary units of finite length implies the determination of 2n integration constants for which a set of linear equations is provided in this article. The analytical method is applied to configurations of increasing complexity. Analytical solutions are compared to numerical results obtained using SUNDAY (a 1D non linear Euler solver in temporal space) and CEDRE (3D Navier-Stokes flow solver). An excellent agreement is found for all configurations thereby showing that acceleration discontinuities at the boundaries between adjacent elements do not influence the actual acoustic transfer functions. The issue of nozzle compactness is addressed. It is found that in the subcritical domain, spectral results should be nondimensionalized using the flow-through-time of the entire nozzle. Doing so, transfer functions of nozzles of different lengths are successfully compared and a compactness criterion is proposed that writes ω*∫0Ldζ/uζ<1 where L is the axial length of the nozzle. Finally, the EWG experimental setup of Bake et al. (JSV 2009) is considered. Analytical results are compared to the results reported by Howe (JFM 2010). Both models give similar trends and show the important role of the rising time of the fluctuating temperature front on the amplitude of the indirect acoustic emission. The experimental temperature profile and the impedance coefficients at the inlet and outlet provided by Bake et al. (JSV 2009) and Leyko et al. (JSV 2011) are introduced into the analytical formulation. Results show that the indirect combustion noise mechanism cannot be held responsible alone for the acoustic emission in the subcritical case.
亚临界喷嘴间接燃烧噪声的分析分析
本文重新研究了有限长度喷管的间接燃烧噪声问题。Moase等人(JFM 2007)提出的间接燃烧噪声分析模型是红源的,并应用于形状日益复杂的亚临界喷嘴。该模型是基于由Marble & Candel (JSV 1977)提出的方程,该方程在亚音速框架下得到了显式解。将喷管离散成n个有限长度的基本单元意味着确定2n个积分常数,本文给出了一组线性方程。分析方法适用于日益复杂的结构。将解析解与使用SUNDAY(一维非线性欧拉求解器)和CEDRE(三维纳维-斯托克斯流求解器)得到的数值结果进行了比较。在所有配置中都发现了一个很好的一致性,从而表明相邻单元之间边界处的加速度不连续并不影响实际的声学传递函数。解决了喷嘴紧凑性的问题。研究发现,在亚临界区域,用整个喷嘴的流动时间对光谱结果进行无量纲化处理。在此基础上,成功地比较了不同长度喷嘴的传递函数,并提出了一个紧凑性判据:ω*∫0Ldζ/uζ<1,其中L为喷嘴的轴向长度。最后,考虑了Bake等人(JSV 2009)的EWG实验设置。分析结果与Howe报告的结果进行了比较(JFM 2010)。两种模式给出了相似的变化趋势,并表明了温度锋上升时间对间接声发射振幅的重要影响。在分析公式中引入了Bake等人(JSV 2009)和Leyko等人(JSV 2011)提供的实验温度分布和进出口阻抗系数。结果表明,在亚临界情况下,间接燃烧噪声机制不能单独对声发射负责。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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