Multi-fidelity aerodynamic reduced-order model based on gating mechanismOA
Multi-fidelity aerodynamic reduced-order model based on gating mechanism
Huailu LI;Zhuo YU;Xu WANG;Weiwei ZHANG
School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,ChinaSchool of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,ChinaDepartment of Mechanical Engineering,The Hong Kong Polytechnic University,Hong Kong 999077,ChinaSchool of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,China
Aerodynamic modelingGating mechanismIncremental learningMulti-fidelity modelMulti-source data fusion
Aerodynamic modelingGating mechanismIncremental learningMulti-fidelity modelMulti-source data fusion
《中国航空学报（英文版）》 2026 (8)
17-32,16
We would like to acknowledge the support of the National Natural Science Foundation of China(Nos.92152301,U2441211).
评论