Funding for this research was provided by:
National Natural Science Foundation of China (52202474)
National Science and Technology Major Project (J2019-I-0020-0019)
Innovation Centre for Advanced Aviation Power (HKCX2022-01-026-829 03)
Fund of Prospective Layout of Scientific Research for NUAA (1002-ILA22037-1A2)
State Key Laboratory of Mechanics and Control for Aerospace Structures (MCAS-S-0323G01)
Article History
Received: 7 August 2023
Revised: 9 January 2024
Accepted: 14 February 2024
First Online: 4 April 2024