Data-Driven Aerodynamic Performance Prediction Architecture with Self-Attention Mechanism

The computational fluid dynamics (CFD) and the wind tunnel test for obtaining aerodynamic performance is expensive and time-consuming. This paper proposed a data-driven aerodynamic performance prediction architecture, which can consider both aerodynamic shapes and flow conditions. The architecture is based on computer vision, which takes the grayscale image of the airfoil and flow conditions as input, learns an end-to-end mapping among the shapes, the flow conditions, and the aerodynamic forces. The flow conditions are considered by an adaptive layer norm and a scale parameter. To explain what the model has learned, attention matrices of different airfoils under different flow conditions are analyzed. Results show that the mean squared errors (MSE) of validation dataset and training dataset both converge to [Formula: see text] orders of magnitude, and in the test dataset, the relative errors between the predicted and the target aerodynamic forces are within 2.5%, which reflects that the model has good accuracy and generalization performance.

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Publication Details

Journal
Journal of Aircraft
Published
2026-04-13
DOI
https://doi.org/10.2514/1.c038852
Primary Topic
Model Reduction and Neural Networks
Type
article
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article

Data-Driven Aerodynamic Performance Prediction Architecture with Self-Attention Mechanism

Z. Chen, Xingya Da, Bei LIU
Journal of Aircraft
Model Reduction and Neural Networks
article

Data-Driven Aerodynamic Performance Prediction Architecture with Self-Attention Mechanism

Z. Chen, Xingya Da, Bei LIU
article en

Abstract

The computational fluid dynamics (CFD) and the wind tunnel test for obtaining aerodynamic performance is expensive and time-consuming. This paper proposed a data-driven aerodynamic performance prediction architecture, which can consider both aerodynamic shapes and flow conditions. The architecture is based on computer vision, which takes the grayscale image of the airfoil and flow conditions as input, learns an end-to-end mapping among the shapes, the flow conditions, and the aerodynamic forces. The flow conditions are considered by an adaptive layer norm and a scale parameter. To explain what the model has learned, attention matrices of different airfoils under different flow conditions are analyzed. Results show that the mean squared errors (MSE) of validation dataset and training dataset both converge to [Formula: see text] orders of magnitude, and in the test dataset, the relative errors between the predicted and the target aerodynamic forces are within 2.5%, which reflects that the model has good accuracy and generalization performance.

Journal of Aircraft
China Aerodynamics Research and Development Center (CN)
Affordable and clean energy
Openalex Percentile: Top 13%
Model Reduction and Neural Networks
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