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Modelling and nonlinear control of aircraft wings flutter by use of piezoelectric patch considering the airfoil shape cross section of the wing beam

Crossref DOI link: https://doi.org/10.1007/s11071-025-11441-4

Published Online: 2025-07-02

Published Print: 2025-10

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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