Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis
Abstract
Reliably forecasting airfoil-generated aerodynamic noise is a prerequisite for designing quieter aircraft and wind turbines. Although machine learning (ML) models deliver strong predictive performance in aeroacoustics tasks, their opaque, "black-box" nature frequently impedes adoption in engineering design processes that demand transparent reasoning. In this work, three ML paradigms—Linear Regression (LR), Random Forest (RF), and Extreme Gradient Boosting (XGB)—are systematically evaluated for airfoil self-noise prediction on the NASA benchmark dataset. Generalization is quantified through 10-fold cross-validation using the coefficient of determination (𝑅²), root mean squared error (RMSE), and mean absolute error (MAE). To overcome the interpretability barrier, SHapley Additive exPlanations (SHAP) is applied, providing both global feature-importance rankings and instance-level explanations of model outputs. XGB attains the highest accuracy, with a cross-validated R² of 0.9498 ± 0.0138, a test R² of 0.9577, and an RMSE of 1.4553 dB. SHAP reveals that frequency, suction-side displacement thickness, and chord length exert the strongest influence on predicted sound pressure levels, whereas angle of attack ranks lowest—an initially surprising result that is nonetheless consistent with the limited angular range covered in the original NASA experiments. These findings illustrate that pairing gradient boosting with explainable AI yields a credible and interpretable prediction framework for aeroacoustic engineering.
Keywords
Ethical Statement
Not applicable.
Thanks
We thank the editor and reviewers in advance for their time and feedback.
References
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Details
Primary Language
English
Subjects
Aerospace Engineering (Other)
Journal Section
Research Article
Early Pub Date
June 6, 2026
Publication Date
June 27, 2026
Submission Date
February 12, 2026
Acceptance Date
April 8, 2026
Published in Issue
Year 2026 Volume: 10 Number: 2
APA
Avşar, R., & Tetik, T. (2026). Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis. Journal of Aviation, 10(2), 291-300. https://doi.org/10.30518/jav.1886935
AMA
1.Avşar R, Tetik T. Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis. JAV. 2026;10(2):291-300. doi:10.30518/jav.1886935
Chicago
Avşar, Reha, and Tuğba Tetik. 2026. “Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study With SHAP Analysis”. Journal of Aviation 10 (2): 291-300. https://doi.org/10.30518/jav.1886935.
EndNote
Avşar R, Tetik T (June 1, 2026) Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis. Journal of Aviation 10 2 291–300.
IEEE
[1]R. Avşar and T. Tetik, “Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis”, JAV, vol. 10, no. 2, pp. 291–300, June 2026, doi: 10.30518/jav.1886935.
ISNAD
Avşar, Reha - Tetik, Tuğba. “Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study With SHAP Analysis”. Journal of Aviation 10/2 (June 1, 2026): 291-300. https://doi.org/10.30518/jav.1886935.
JAMA
1.Avşar R, Tetik T. Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis. JAV. 2026;10:291–300.
MLA
Avşar, Reha, and Tuğba Tetik. “Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study With SHAP Analysis”. Journal of Aviation, vol. 10, no. 2, June 2026, pp. 291-00, doi:10.30518/jav.1886935.
Vancouver
1.Reha Avşar, Tuğba Tetik. Explainable Machine Learning for Airfoil Self-Noise Prediction: A Comparative Study with SHAP Analysis. JAV. 2026 Jun. 1;10(2):291-300. doi:10.30518/jav.1886935