Supersonic aircraft aerodynamic performance prediction based on machine learning approach
Year: 2025
Type: article
Abstract: This study proposes a novel approach that integrates machine learning algorithms with computational fluid dynamics (CFD) simulations to efficiently predict the aerodynamic performance of supersonic aircraft under cruising flight conditions. Three intelligent models were evaluated based on their principles, advantages, and limitations and then applied to predict the aerodynamic performance of a reference supersonic passenger aircraft. Bayesian optimization algorithms were employed on the selected models to enhance prediction accuracy. The performance metrics show that the proposed models can accurately predict supersonic aerodynamics under various flight conditions. In particular, the XGBoost model has the highest predictive accuracy for lift and drag coefficients, and the Bagging model is excellent at predicting the pitch moment coefficient. Machine learning-based prediction methods are more efficient than traditional CFD simulations, providing faster results without sacrificing accuracy. Moreover, Shapley Additive explanation was applied to the optimal model, which improves interpretability and offers deeper insights into the aerodynamic optimization of supersonic aircrafts.
Source: AIP Advances
DOI: 10.1063/5.0282257
Authors: Qijia Liu, Jiechao Zhang, Yao Zheng, Yaolong Liu
Institution: Zhejiang University
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: gold
Estimated APC paid: $1,350
Awards: G577159267, G6238685976
OpenAlex ID: W4413263466
