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Authors
Dong, Hao
Zhang, Qing-Hua
Zhao, Xiao-Long
Yuan, Bing
Hou, Xiang-Ying
Jin, Guang-Hu
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Funding
Funding for this research was provided by:
National Key Laboratory of Helicopter Aeromechanics (2024-ZSJ-LB-03-01)
National Natural Science Foundation of China (52375062)
National Natural Science Foundation of China (52305501)
Natural Science Basic Research Program of Shaanxi (2025JC-YBMS-399)
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Article History
Received: 30 January 2026
Revised: 19 April 2026
Accepted: 20 May 2026
First Online: 8 June 2026
Declarations
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: The authors declare no competing interests.
