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Authors
Zhou, Wei
Zhou, Linzhen
Yuan, Tiejun
Chen, Ronghua
Liu, Dakun
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Funding
Funding for this research was provided by:
National Natural Science Foundation of China: Research on the Stability and Bifurcation Behavior of Helicopter System Aerolastic Response (No.11702240)
National Natural Science Foundation of China: Research on the Physical Mechanism and Method of Dynamic Instability of Helicopter Rotor/Fuselage Coupling (No.11547215)
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Article History
Received: 8 August 2025
Accepted: 10 December 2025
First Online: 6 January 2026
Declarations
:
: The authors declare no competing interests.
