A hybrid machine learning framework for predicting aircraft scaled sound pressure levels: a comparative study

Abstract Aircraft noise was among the significant environmental challenges, given increased air traffic affects communities and raises health concerns. Accurate noise prediction is indispensable for designing quieter aircraft and mitigation strategies supporting sustainable aviation practices. In this regard, this study aimed to develop a scalable hybrid machine learning framework to predict aircraft scaled sound pressure levels (SPL). Four models (Extra Tree, AdaBoost, Gradient Boosting, and Histogram-Based Gradient Boosting) were evaluated. The best-performing model is an Extra Tree with an R 2 of 0.9542 and the minimum mean squared error (MSE) of 3.12. Optimization algorithms were performed to improve its accuracy and robustness—JAYA, Enhanced AEO, Levy JAYA, and JADE—which decreased MSE up to 20% for ensuring stable convergence within the first 300 epochs. JAYA and Enhanced AEO had the best results, balancing accuracy and computation efficiency. Optimized models increased the runtime by 20–30% and memory usage by 15%, which makes them fit for offline applications. Under the computational trade-off conditions, the hybrid models revealed a high potential for further improving the accuracy of the noise prediction. The proposed machine learning framework has really given actionable insight into optimizing aircraft design for noise reduction with a minimum loss in their aerodynamic efficiencies. Prediction of the sound pressure level of key parameters, such as the angle of attack, Reynolds number, and surface roughness, contributes to developing effective noise mitigation strategies, including regulatory compliance with sustainability of aviation. The flexibility extends to a range of aircraft components, with quieter and efficient design seriously threatened by environmental and community noise concerns. While the models demonstrated scalability and high accuracy, further refinements are needed to enhance real-time performance and integrate subjective noise metrics, broadening their applicability to diverse aviation noise management scenarios.

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Publication Details

Journal
Journal of Engineering and Applied Science
Published
2025-09-23
DOI
https://doi.org/10.1186/s44147-025-00714-9
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
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article

A hybrid machine learning framework for predicting aircraft scaled sound pressure levels: a comparative study

Han Sheng, Guo Li
Journal of Engineering and Applied Science
Aerodynamics and Acoustics in Jet Flows
article

A hybrid machine learning framework for predicting aircraft scaled sound pressure levels: a comparative study

Han Sheng, Guo Li
article en

Abstract

Abstract Aircraft noise was among the significant environmental challenges, given increased air traffic affects communities and raises health concerns. Accurate noise prediction is indispensable for designing quieter aircraft and mitigation strategies supporting sustainable aviation practices. In this regard, this study aimed to develop a scalable hybrid machine learning framework to predict aircraft scaled sound pressure levels (SPL). Four models (Extra Tree, AdaBoost, Gradient Boosting, and Histogram-Based Gradient Boosting) were evaluated. The best-performing model is an Extra Tree with an R 2 of 0.9542 and the minimum mean squared error (MSE) of 3.12. Optimization algorithms were performed to improve its accuracy and robustness—JAYA, Enhanced AEO, Levy JAYA, and JADE—which decreased MSE up to 20% for ensuring stable convergence within the first 300 epochs. JAYA and Enhanced AEO had the best results, balancing accuracy and computation efficiency. Optimized models increased the runtime by 20–30% and memory usage by 15%, which makes them fit for offline applications. Under the computational trade-off conditions, the hybrid models revealed a high potential for further improving the accuracy of the noise prediction. The proposed machine learning framework has really given actionable insight into optimizing aircraft design for noise reduction with a minimum loss in their aerodynamic efficiencies. Prediction of the sound pressure level of key parameters, such as the angle of attack, Reynolds number, and surface roughness, contributes to developing effective noise mitigation strategies, including regulatory compliance with sustainability of aviation. The flexibility extends to a range of aircraft components, with quieter and efficient design seriously threatened by environmental and community noise concerns. While the models demonstrated scalability and high accuracy, further refinements are needed to enhance real-time performance and integrate subjective noise metrics, broadening their applicability to diverse aviation noise management scenarios.

Journal of Engineering and Applied ScienceVol. 72(1)
Beijing Union University (CN), University of Electronic Science and Technology of China (CN), National Engineering Research Center of Electromagnetic Radiation Control Materials (CN)
Openalex Percentile: Top 66%
Aerodynamics and Acoustics in Jet Flows
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