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Authors
Li, Shancheng
Wang, Yong
Huang, Bo
Zhang, Haibo
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Funding
Funding for this research was provided by:
National Natural Science Foundation of China (52202474)
State Key Laboratory of Mechanics and Control for Aerospace Structures (MCAS-S-0323G01)
Advanced aerodynamics innovation workstation project (HKCX2022-01-026-03)
China Postdoctoral Science Foundation (2023M731655)
Funds for basic scientific research in central universities (NT2023004)
Nanjing University of Aeronautics and Astronautics prospective layout research project (1002-ILA22037-1A22)
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Article History
Received: 28 February 2024
Revised: 15 May 2025
Accepted: 28 May 2025
First Online: 2 July 2025
Declarations
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: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
