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Multi-fidelity aerodynamic reduced-order model based on gating mechanism

Huailu LI Zhuo YU Xu WANG Weiwei ZHANG

中国航空学报（英文版）2026，Vol.39Issue(8)：17-32,16.

中国航空学报（英文版）2026，Vol.39Issue(8)：17-32,16.DOI:10.1016/j.cja.2025.104055

Huailu LI ¹Zhuo YU ¹Xu WANG ²Weiwei ZHANG¹

作者信息

1. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,China
2. Department of Mechanical Engineering,The Hong Kong Polytechnic University,Hong Kong 999077,China
折叠

Aerodynamic modeling/Gating mechanism/Incremental learning/Multi-fidelity model/Multi-source data fusion

Aerodynamic modeling/Gating mechanism/Incremental learning/Multi-fidelity model/Multi-source data fusion

Huailu LI,Zhuo YU,Xu WANG,Weiwei ZHANG..Multi-fidelity aerodynamic reduced-order model based on gating mechanism[J].中国航空学报（英文版）,2026,39(8):17-32,16.

We would like to acknowledge the support of the National Natural Science Foundation of China(Nos.92152301,U2441211). （Nos.92152301,U2441211）

ISSN：1000-9361

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