Iván Padilla-Montero, Daniel Rodríguez, Vincent Jaunet, Peter Jordan
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While the latter field is dominated by a broad range of vortical fluctuations in the turbulent mixing region of unheated high-speed jets, the momentum potential field is governed by fluctuations which are intimately related to acoustic emission, and its spatial structure in the frequency domain is very organized. The proposed methodology in this paper improves the technique of Prasad and Gaitonde (J Fluid Mech 940:1–11, 2022) in three new ways. First, the solution of the Poisson equation is carried out in the frequency-wavenumber domain instead of the time-space domain, which simplifies and integrates the solution of the Poisson equation within the SPOD framework based on momentum potential fluctuations. Second, the issue of solving the Poisson equation on a finite domain with <i>ad hoc</i> boundary conditions is explicitly addressed, identifying and removing those unphysical harmonic components introduced in the solution process. Third, the solution of the SPOD problem in terms of momentum potential fluctuations is used to reconstruct schlieren SPOD fields associated with each mode, allowing the visualization of the obtained coherent structures also in terms of the density gradient. The method is applied here to schlieren images of a twin-jet configuration with a small jet separation at two supersonic operation conditions: a perfectly-expanded and an overexpanded one. The SPOD modes based on momentum potential fluctuations retain the wavepacket structure including the direct Mach-wave radiation, together with upstream- and downstream-traveling acoustic waves, similar to SPOD modes based on the schlieren images. However, for the same dataset, they result in a lower-rank decomposition than schlieren-based SPOD and provide an effective separation of twin-jet fluctuations into independent toroidal and flapping oscillations that are recovered as different SPOD modes. These coherent structures are more consistent with twin-jet wavepacket models available in the literature than those originally obtained with direct schlieren-based SPOD, facilitating their interpretation and comparison against theoretical analyses.\n</p>","PeriodicalId":795,"journal":{"name":"Theoretical and Computational Fluid Dynamics","volume":"38 3","pages":"375 - 401"},"PeriodicalIF":2.2000,"publicationDate":"2024-05-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://link.springer.com/content/pdf/10.1007/s00162-024-00699-w.pdf","citationCount":"0","resultStr":"{\"title\":\"Eduction of coherent structures from schlieren images of twin jets using SPOD informed with momentum potential theory in the spectral domain\",\"authors\":\"Iván Padilla-Montero, Daniel Rodríguez, Vincent Jaunet, Peter Jordan\",\"doi\":\"10.1007/s00162-024-00699-w\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p>This work presents a methodology to extract coherent structures from high-speed schlieren images of turbulent twin jets which are more physically interpretable than those obtained with currently existing techniques. 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引用次数: 0
摘要
本研究提出了一种从湍流孪生射流的高速离散图像中提取相干结构的方法,与现有技术相比,这种方法更能从物理角度解释湍流孪生射流。最近,Prasad 和 Gaitonde(J Fluid Mech 940:1-11,2022 年)介绍了一种方法,该方法采用 Doak 的动量势理论(J Sound Vib 131(1):67-90,1989 年),通过求解泊松方程从 Schlieren 图像中计算势能(声能和热能)波动,并将其与光谱正交分解(SPOD)相结合,从动量势场而非原始 Schlieren 场中提取相干结构。在未加热的高速喷流的湍流混合区域,后一种场受广泛的涡旋波动支配,而动量势场则受与声发射密切相关的波动支配,其频域空间结构非常有条理。本文提出的方法从三个方面改进了 Prasad 和 Gaitonde 的技术(J Fluid Mech 940:1-11, 2022)。首先,泊松方程的求解是在频率-波数域而非时空域中进行的,这简化并整合了基于动量势能波动的 SPOD 框架内的泊松方程求解。其次,明确解决了在有限域上利用特设边界条件求解泊松方程的问题,识别并消除了求解过程中引入的非物理谐波成分。第三,用动量势能波动求解 SPOD 问题,重建与每种模式相关的离层 SPOD 场,使获得的相干结构在密度梯度方面也可视化。该方法适用于在两种超音速运行条件(完全膨胀和过度膨胀)下具有较小射流分离的双射流配置的离散图像。基于动量势能波动的 SPOD 模式保留了波包结构,包括直接的马赫波辐射,以及上游和下游传播的声波,这与基于裂片图像的 SPOD 模式相似。然而,对于相同的数据集,它们的分解阶数比基于施利连的 SPOD 低,并能有效地将双喷流波动分离为独立的环状振荡和拍击振荡,这些振荡被复原为不同的 SPOD 模式。这些相干结构与文献中已有的双喷流波包模型相比,更符合最初用基于schlieren的直接SPOD方法得到的结果,便于解释和与理论分析进行比较。
Eduction of coherent structures from schlieren images of twin jets using SPOD informed with momentum potential theory in the spectral domain
This work presents a methodology to extract coherent structures from high-speed schlieren images of turbulent twin jets which are more physically interpretable than those obtained with currently existing techniques. Recently, Prasad and Gaitonde (J Fluid Mech 940:1–11, 2022) introduced an approach which employs the momentum potential theory of Doak (J Sound Vib 131(1):67–90, 1989) to compute potential (acoustic and thermal) energy fluctuations from the schlieren images by solving a Poisson equation, and combines it with spectral proper orthogonal decomposition (SPOD) to educe coherent structures from the momentum potential field instead of the original schlieren field. While the latter field is dominated by a broad range of vortical fluctuations in the turbulent mixing region of unheated high-speed jets, the momentum potential field is governed by fluctuations which are intimately related to acoustic emission, and its spatial structure in the frequency domain is very organized. The proposed methodology in this paper improves the technique of Prasad and Gaitonde (J Fluid Mech 940:1–11, 2022) in three new ways. First, the solution of the Poisson equation is carried out in the frequency-wavenumber domain instead of the time-space domain, which simplifies and integrates the solution of the Poisson equation within the SPOD framework based on momentum potential fluctuations. Second, the issue of solving the Poisson equation on a finite domain with ad hoc boundary conditions is explicitly addressed, identifying and removing those unphysical harmonic components introduced in the solution process. Third, the solution of the SPOD problem in terms of momentum potential fluctuations is used to reconstruct schlieren SPOD fields associated with each mode, allowing the visualization of the obtained coherent structures also in terms of the density gradient. The method is applied here to schlieren images of a twin-jet configuration with a small jet separation at two supersonic operation conditions: a perfectly-expanded and an overexpanded one. The SPOD modes based on momentum potential fluctuations retain the wavepacket structure including the direct Mach-wave radiation, together with upstream- and downstream-traveling acoustic waves, similar to SPOD modes based on the schlieren images. However, for the same dataset, they result in a lower-rank decomposition than schlieren-based SPOD and provide an effective separation of twin-jet fluctuations into independent toroidal and flapping oscillations that are recovered as different SPOD modes. These coherent structures are more consistent with twin-jet wavepacket models available in the literature than those originally obtained with direct schlieren-based SPOD, facilitating their interpretation and comparison against theoretical analyses.
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.