A data-driven approach for robust wing jig shape design

This paper presents a data-driven robust jig shape design process, providing an initial application case to understand the opportunities of accounting for the implement of uncertainty optimization to a real industrial use case. The study utilizes an industrially relevant data set defined for academic usage, which includes both variations of aerodynamic performance (Lift/Drag improvement)and structural loads (Shear, Moment, and Torque)with the variations of wing twist and structural stiffness parameters. The objective is optimizing the wing jig shape in the presence of uncertainties in structural stiffness, aiming to balance the confidence of achieving aero dynamic performance targets and the risks of exceeding the design loads margins. Firstly, Gaussian Process Emulators are constructed based on given dataset to represent the relationship between aerodynamic performance as well as loads and input uncertain parameters. Then, aero performance and loads analysis are conducted separately to evaluate the impact of target improvements and design load margins on uncertainty optimization solutions. Finally, Non-dominated Sorting Genetic Algorithm II is employed to determine the optimal jig twist that satisfy various optimization objectives, effectively managing the trade-offs between aero performance and structural safety under stiffness uncertainties.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2025-12-01
DOI
https://doi.org/10.1016/j.cja.2025.104052
Primary Topic
Probabilistic and Robust Engineering Design
Type
article
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article

A data-driven approach for robust wing jig shape design

Xiaohui Ao, Huanxiong Xia, Jonathan COOPER, Jian ZHANG et al.
Chinese Journal of Aeronautics
Probabilistic and Robust Engineering Design
article

A data-driven approach for robust wing jig shape design

Xiaohui Ao, Huanxiong Xia, Jonathan COOPER, Jian ZHANG, Jianhua LIU, Long LIU
article en

Abstract

This paper presents a data-driven robust jig shape design process, providing an initial application case to understand the opportunities of accounting for the implement of uncertainty optimization to a real industrial use case. The study utilizes an industrially relevant data set defined for academic usage, which includes both variations of aerodynamic performance (Lift/Drag improvement)and structural loads (Shear, Moment, and Torque)with the variations of wing twist and structural stiffness parameters. The objective is optimizing the wing jig shape in the presence of uncertainties in structural stiffness, aiming to balance the confidence of achieving aero dynamic performance targets and the risks of exceeding the design loads margins. Firstly, Gaussian Process Emulators are constructed based on given dataset to represent the relationship between aerodynamic performance as well as loads and input uncertain parameters. Then, aero performance and loads analysis are conducted separately to evaluate the impact of target improvements and design load margins on uncertainty optimization solutions. Finally, Non-dominated Sorting Genetic Algorithm II is employed to determine the optimal jig twist that satisfy various optimization objectives, effectively managing the trade-offs between aero performance and structural safety under stiffness uncertainties.

Chinese Journal of Aeronautics
Beijing Institute of Technology (CN), North China University of Science and Technology (CN), Tangshan College (CN), University of Bristol (GB)
Industry, innovation and infrastructure
Openalex Percentile: Top 28%
Probabilistic and Robust Engineering Design
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