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 R2 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.

Details

Title
A hybrid machine learning framework for predicting aircraft scaled sound pressure levels: a comparative study
Author
Li, Guo 1 ; Sheng, Hongyu 2 

 University of Electronic Science and Technology of China, State Key Laboratory of Electronic Thin Films and Integrated Devices, Chengdu, China (GRID:grid.54549.39) (ISNI:0000 0004 0369 4060) 
 Beijing Union University, College of Robotics, Beijing, China (GRID:grid.411618.b) (ISNI:0000 0001 2214 9197) 
Pages
163
Publication year
2025
Publication date
Dec 2025
Publisher
Springer Nature B.V.
ISSN
11101903
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
3253211250
Copyright
© The Author(s) 2025. This work is published under http://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.