Abstract
This paper aims to investigate the nonlinear forced vibration characteristics of hybrid fiber/graphene nanoplatelets/polymer composite sandwich cylindrical shells with hexagon honeycomb core (HHC) in a hygrothermal environment. Firstly, an analytical model for such shells is proposed, where the equivalent material parameters of skins are determined based on the law of the mixture and homogenization approach, and the improved Gibson's technique is adopted to estimate the equivalent material properties of HHC. Furthermore, the first-order shear deformation theory together with von Kármán geometric nonlinearity terms and Hamilton’s principle is utilized to obtain the nonlinear governing equations that consider the effect of hygrothermal and mechanical loads, which are further discretized into a series of ordinary differential equations via the Galerkin approach. Subsequently, the static condensation technique and the multiple scale method are utilized to solve the nonlinear forced vibration responses, including primary, super- and sub-harmonic resonances. The results obtained by the present model are compared to the ones from the literature to prove the effectiveness of the proposed model. Also, the influences of key parameters on the nonlinear dynamic performance of the structure are evaluated, with some critical conclusions related to reducing the nonlinear resonance amplitude and resonance region of the structure being summarized.
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Acknowledgements
This study was supported by the National Natural Science Foundation of China (Grant Nos. 52175079 and 12072091); the Science Foundation of the National Key Laboratory of Science and Technology on Advanced Composites in Special Environments (Grant No. 6142905192512); the Fundamental Research Funds for the Central Universities of China (Grant No. N2103026); the Major Projects of Aero-Engines and Gas Turbines (J2019-I-0008-0008); the China Postdoctoral Science Foundation (2020M680990).
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Appendices
Appendix A
The parameter values of \(H_{ij} \left( {i = 1, \, 2, \ldots ,5; \, j = 1, \, 2, \ldots 11} \right),S_{xy} \left( {x = u, \, v, \, w, \, \varphi , \, \theta ; \, y = u, \, v, \, \varphi , \, \theta } \right)\), Hnon2 and Hnon3 in Eqs. (26), (27), (28), (29) and (30) are stated as:
Appendix B
The coefficient expressions \(d_{i} \left( {i = 0, \, 1, \ldots ,4} \right)\) in Eq. (34) are formulated as:
Appendix C
Based on super-harmonic resonance, Eq. (36) can be re-written as:
By substituting Eqs. (54), (38), (39), (40) and (41) into Eq. (C1) and setting the coefficient of each order perturbation parameter to be zero.
In the first step, the general solution of Eq. (C2) can be obtained in the form of:
where
Then, by taking Eq. (C4) into Eq. (C3), one can obtain:
Finally, to eliminate secular terms in Eq. (C6), Eq. (55) can be obtained.
Appendix D
Based on sub-harmonic resonance, Eq. (36) can be also re-written as:
By substituting Eqs. (57), (38), (39), (40) and (40) into Eq. (D1) and setting the coefficient of each order perturbation parameter to be zero.
In the first step, the general solution of Eq. (D2) can be obtained in the form of:
where
Then, by taking Eq. (D4) into Eq. (D3), one can obtain:
Finally, to eliminate secular terms in Eq. (D6), Eq. (58) can be obtained.
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Dong, B., Li, H., Wang, X. et al. Nonlinear forced vibration of hybrid fiber/graphene nanoplatelets/polymer composite sandwich cylindrical shells with hexagon honeycomb core. Nonlinear Dyn 110, 3303–3331 (2022). https://doi.org/10.1007/s11071-022-07811-x
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DOI: https://doi.org/10.1007/s11071-022-07811-x