A physics merged deep neural network-based prediction method for jet turbulent mixing noise

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2024-01-25 DOI:10.1177/1475472x241230652
Baohong Bai, Yingzhe Zhang, Xiaodong Li, Junhui Gao
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Abstract

Turbulent mixing noise is a vital component of jet noise, and its rapid, accurate prediction has always been persistently pursued. Recent advancement in machine learning has been applied to jet noise prediction. However, these applications are pure curve fitting and lack physical constraints. In this study, a physics-merged deep neural network (PMNN)-based prediction method was developed for turbulent mixing jet noise by merging the physics of the jet noise. This deep neural network (DNN)-based method employed recent advancements in jet turbulent mixing noise containing large- and fine-scale turbulence structures. Two simple rational functions for large- and fine-scale turbulent noise similarity spectra were proposed to replace the original complex similarity spectra functions and incorporated into the DNN-based prediction method. For comparison, we present two data-driven DNN-based prediction methods (DDNN). The first DDNN method used the sound pressure level (SPL) as the output of neural networks, directly establishing the nonlinear relationship between the input features and SPL. In the second DDNN method, the dominant modes of the jet noise spectra extracted using the proper orthogonal decomposition method were merged with DNN. These DNN-based methods were then trained using a set of experimental data over a wide range of jet operating conditions. Their performance was evaluated and compared. It was evident that all these DNN-based methods were capable of predicting turbulent mixing noise reasonably well. In contrast to the DDNN methods, the PMNN method could provide insights into the jet turbulent mixing noise components. It demonstrates that the turbulent mixing jet noise spectra at the mid polar angle is generated by the large-scale noise component at low-frequency range and by the fine-scale noise component at high-frequency range.
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基于物理合并深度神经网络的喷气湍流混合噪声预测方法
湍流混合噪声是喷气噪声的重要组成部分,对其进行快速、准确的预测一直是人们的不懈追求。机器学习的最新进展已被应用于喷气噪声预测。然而,这些应用都是纯粹的曲线拟合,缺乏物理约束。在本研究中,通过合并喷气噪声的物理特性,针对湍流混合喷气噪声开发了一种基于物理合并深度神经网络(PMNN)的预测方法。这种基于深度神经网络(DNN)的方法采用了包含大尺度和细尺度湍流结构的喷气湍流混合噪声的最新进展。我们为大尺度和细尺度湍流噪声相似谱提出了两个简单的合理函数,以取代原来的复杂相似谱函数,并将其纳入基于 DNN 的预测方法。为了进行比较,我们提出了两种基于数据驱动的 DNN 预测方法(DDNN)。第一种 DDNN 方法使用声压级(SPL)作为神经网络的输出,直接建立了输入特征与声压级之间的非线性关系。在第二种 DDNN 方法中,使用适当的正交分解方法提取的喷气噪声频谱的主导模式与 DNN 合并。这些基于 DNN 的方法随后使用一组在各种喷气工作条件下的实验数据进行了训练。对它们的性能进行了评估和比较。显然,所有这些基于 DNN 的方法都能很好地预测湍流混合噪声。与 DDNN 方法不同的是,PMNN 方法可以深入了解射流湍流混合噪声成分。它证明了中极角的湍流混合射流噪声谱是由低频范围的大尺度噪声分量和高频范围的细尺度噪声分量产生的。
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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