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Authors
Mo, Senkai
Yu, Kaiping
Zhao, Rui
Li, Jinze
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Funding
Funding for this research was provided by:
National Natural Science Foundation of China (12272105, 12102103)
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Article History
Received: 11 April 2024
Accepted: 27 May 2025
First Online: 16 June 2025
Declarations
:
: The authors declare no competing interests.
: Ch(t1), Cα(t1) and Cβ(t1) in Eq. () are given bywhere the Wagner function ϕ(t1) is given by Jone’s approximationwith the constants A1 = 0.165, A2 = 0.335, b1 = 0.0455, and b2 = 0.3. The coefficients T1, T2, …, T13 are introduced by Theodorsen and detailed in Ref. [].
: Equation () is an integro-differential equation system. In order to eliminate the integral terms, two new variables are introduced:According to Eqs. (), (), (), (), () and (), the aeroelastic system can be expressed in the form of Eq. () withParameters in above matrices are listed as
