Fluid Mechanics and Flight Mechanics

Airfoil icing and aerodynamic characteristics prediction based on multi-task learning

  • Huizhu XIN ,
  • Chen LI ,
  • Weimin SANG ,
  • Liang HOU
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  • 1.School of Aeronautics,Northwestern Polytechnical University,Xi’an 710072,China
    2.National Key Laboratory of Aircraft Configuration Design,Xi’an 710072,China
    3.Shanghai Satellite Engineering Research Institute,Shanghai 201109,China

Received date: 2025-10-28

  Revised date: 2025-11-17

  Accepted date: 2025-12-15

  Online published: 2025-12-29

Supported by

Open Fund of Key Laboratory of Icing and Anti/De-icing(IADL20230302);National Natural Science Foundation of China(12572270);The “1-0” Major Engineering Science Problem Project of Northwestern Polytechnical University(G2024KY0613)

Abstract

To address the problem of limited accuracy in single-task learning for airfoil icing prediction and the difficulty in simultane-ously obtaining icing morphology and aerodynamic characteristics, a multi-task learning based airfoil icing prediction framework called MTAF (Multi-Task Airfoil Former) is proposed. The framework employs an encoder-decoder architecture that extracts deep representations of airfoil geometry and flight conditions through a shared feature encoder, realizes feature fusion and task interaction via a task correlation module, and accomplishes icing prediction and aerodynamic coefficient prediction respectively through dedicated prediction heads. The performance of Transformer and ConvNeXt backbone net-works within this framework is comparatively studied. Based on training and testing with 625 NACA 2412 airfoil samples, results demonstrate that the Transformer architecture achieves pixel accuracy of 99.79% and coefficient of determination for 0.990 6 in icing prediction tasks, significantly outperforming 99.50% and 0.977 2 of ConvNeXt. For aerodynamic coefficient prediction, Transformer achieves coefficient of determination values of 0.975 4 for lift coefficient and 0.987 4 for drag coefficient, which are comparable to 0.973 3 and 0.990 1 of ConvNeXt, respectively, with each architecture showing distinct advantages. The MTAF framework maintains stable prediction performance across different icing types and various flight conditions, providing a high-precision prediction tool for airfoil icing engineering applications.

Cite this article

Huizhu XIN , Chen LI , Weimin SANG , Liang HOU . Airfoil icing and aerodynamic characteristics prediction based on multi-task learning[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2026 , 47(16) : 132983 -132983 . DOI: 10.7527/S1000-6893.2025.32983

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