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

Authors :
Bai, Baohong
Zhang, Yingzhe
Li, Xiaodong
Gao, Junhui
Source :
International Journal of Aeroacoustics. Jun2024, Vol. 23 Issue 3/4, p363-385. 23p.
Publication Year :
2024

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. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
1475472X
Volume :
23
Issue :
3/4
Database :
Academic Search Index
Journal :
International Journal of Aeroacoustics
Publication Type :
Academic Journal
Accession number :
177178734
Full Text :
https://doi.org/10.1177/1475472X241230652