Modelling rectangular-jet screech via dimensional reduction

IF 3.4 3区 工程技术 Q2 MECHANICS
Grant Lu, Jayson Beekman, Soudeh Mazharmanesh, Daniel Edgington-Mitchell, Petrônio Nogueira
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引用次数: 0

Abstract

This work presents a linear stability analysis of the waves involved in the screech resonance loop generated within a rectangular supersonic jet. Linear stability analysis of rectangular jets has often been performed using a planar-jet approximation, due to the significant reduction in complexity and computational cost. However, the impact of this simplification on the predictive power of the stability model has not been considered in detail thus far. In this work, the predictions of both a simplified planar model and a more representative two-dimensional model are compared for two waves of particular relevance to jet noise. These waves are the downstream-propagating Kelvin-Helmholtz (KH) instability, and the upstream-propagating guided-jet mode (GJM). Disparity in the predicted wavenumber for both waves is considered, as well as disparities in the KH growth rate, and the GJM band of existence. A parametric sweep through nozzle-pressure ratio is performed for rectangular jets with aspect ratios ranging from a square jet with \(\textrm{AR}=1\) to an \(\textrm{AR}=8\) rectangular jet. It is demonstrated that the KH wavenumber can be well approximated by a planar model for rectangular geometries with an aspect ratio as low as 2. The growth rate is more sensitive, but for \(\textrm{AR} \ge 4\) the differences between the two models are negligible. In contrast to the KH waves, the band of existence of the GJM, defined as the frequency range between the mode’s branch and saddle points, shows significant dependence on the modelling approach. For higher aspect ratios, the planar model can reasonably predict the saddle point of the GJM, but the predicted branch point of the GJM differs significantly from that predicted by the two-dimensional model. Performing the analysis about an experimentally derived mean-flow profile demonstrates that the predictions for the GJM are sensitive to small changes in the flow profile, with both branch and saddle points showing a strong dependence on the thickness of the shear layer. In all cases tested, the two-dimensional model predicts a much narrower band of frequencies over which the GJM is supported by the flow, as compared to the planar model. To verify the predictions made from the two models, screech frequency predictions are made using the modified weakest-link model and compared to experimental data. The planar model, though it overpredicts the band of existence of the GJM, still produces correct predictions of screech frequency. The two-dimensional model, when linearized about the experimental mean flow, also correctly predicts the screech tones, though performs no better than the planar model.

矩形射流啸叫的降维建模
这项工作提出了在矩形超音速射流中产生的尖叫共振回路所涉及的波的线性稳定性分析。矩形射流的线性稳定性分析通常使用平面射流近似进行,因为它大大降低了复杂性和计算成本。然而,到目前为止,这种简化对稳定性模型预测能力的影响尚未得到详细考虑。在这项工作中,简化平面模型和更具代表性的二维模型的预测对与射流噪声特别相关的两种波进行了比较。这些波分别是下游传播的Kelvin-Helmholtz (KH)不稳定性和上游传播的导射流模式(GJM)。考虑了两种波的预测波数的差异,以及KH增长率和GJM存在波段的差异。对宽高比范围从方形射流\(\textrm{AR}=1\)到矩形射流\(\textrm{AR}=8\)的矩形射流进行了参数化扫描。结果表明,对于宽高比低至2的矩形几何,KH波数可以用平面模型很好地近似。增长率更为敏感,但对于\(\textrm{AR} \ge 4\),两个模型之间的差异可以忽略不计。与KH波相反,GJM的存在频带(定义为模态分支点和鞍点之间的频率范围)与建模方法有很大的相关性。在高纵横比条件下,平面模型能较好地预测GJM的鞍点,但与二维模型预测的GJM分支点存在较大差异。对实验导出的平均流剖面的分析表明,GJM的预测对流剖面的微小变化很敏感,分支点和鞍点都对剪切层的厚度有很强的依赖性。在所有测试的情况下,与平面模型相比,二维模型预测的GJM受气流支持的频率范围要窄得多。为了验证两种模型的预测结果,采用改进的最弱链接模型进行了尖叫频率预测,并与实验数据进行了比较。平面模型虽然过度预测了GJM的存在频带,但仍能正确预测出尖叫频率。在对实验平均流量进行线性化后,二维模型也能正确地预测出尖叫音调,但效果并不比平面模型好。
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来源期刊
CiteScore
5.80
自引率
2.90%
发文量
38
审稿时长
>12 weeks
期刊介绍: Theoretical and Computational Fluid Dynamics provides a forum for the cross fertilization of ideas, tools and techniques across all disciplines in which fluid flow plays a role. The focus is on aspects of fluid dynamics where theory and computation are used to provide insights and data upon which solid physical understanding is revealed. We seek research papers, invited review articles, brief communications, letters and comments addressing flow phenomena of relevance to aeronautical, geophysical, environmental, material, mechanical and life sciences. Papers of a purely algorithmic, experimental or engineering application nature, and papers without significant new physical insights, are outside the scope of this journal. For computational work, authors are responsible for ensuring that any artifacts of discretization and/or implementation are sufficiently controlled such that the numerical results unambiguously support the conclusions drawn. Where appropriate, and to the extent possible, such papers should either include or reference supporting documentation in the form of verification and validation studies.
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