Nonlinear vibration analysis of fiber metal laminated plates with multiple viscoelastic layers

dc.contributor.authorLi, Hui
dc.contributor.authorLi, Zelin
dc.contributor.authorSafaei, Babak
dc.contributor.authorRong, Wanchong
dc.contributor.authorWang, Wenyu
dc.contributor.authorQin, Zhaoye
dc.contributor.authorXiong, Jian
dc.date.accessioned2026-02-06T18:43:13Z
dc.date.issued2021
dc.departmentDoğu Akdeniz Üniversitesi
dc.description.abstractTo accurately predict the vibration behaviors of multiple viscoelastic-layered fiber metal laminated plates (MVFMLPs) under different external excitation levels, an analytical model accounting for both material and geometric nonlinearities is proposed in this paper. Firstly, by employing the Jones-Nelson nonlinear material theory together with the polynomial method and the energy-based strain energy principle, the nonlinear material properties of fiber and viscoelastic layers are expressed as functions of dimensionless strain energy density. Then, the equations of motion for MVFMLPs are derived considering the nonlinear strain- displacement relations of von Karman type. After the determination approach and procedure of the material fitting coefficients and Ritz parameters are clarified, vibration experiments on three MVFMLP specimens are undertaken to validate the developed model as well as evaluate the nonlinear vibration characteristics experimentally. Both theoretical and measured results indicate that the increase of base excitation amplitude not only leads to the perk swerve phenomenon in the frequency-response curves of MVFMLPs, but also causes the complex changes in the natural frequencies and damping parameters due to the coupling influence of two types of nonlinear factors.
dc.description.sponsorshipNational Natural Science Foundation of China [52175079, 51505070, 11972204]; Science Foundation of National key laboratory of science and technology on advanced composites in special environments; Harbin Institute of Technology [6142905192512]; Fundamental Research Funds for the Central Universities of China [N2103026]; major projects of aero-engines and gas turbines [J2019I-0008-0008]; China Postdoctoral Science Foundation [2020M680990]
dc.description.sponsorshipThis study was supported by the National Natural Science Foundation of China (Grant Nos. 52175079, 51505070 and 11972204); the Science Foundation of National key laboratory of science and technology on advanced composites in special environments, Harbin Institute of Technology (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 (Grant No. J2019I-0008-0008); the China Postdoctoral Science Foundation (Grant No. 2020M680990).
dc.identifier.doi10.1016/j.tws.2021.108297
dc.identifier.issn0263-8231
dc.identifier.issn1879-3223
dc.identifier.orcid0000-0002-1675-4902
dc.identifier.scopus2-s2.0-85113492050
dc.identifier.scopusqualityQ1
dc.identifier.urihttps://doi.org/10.1016/j.tws.2021.108297
dc.identifier.urihttps://hdl.handle.net/11129/13499
dc.identifier.volume168
dc.identifier.wosWOS:000704528700002
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherElsevier Sci Ltd
dc.relation.ispartofThin-Walled Structures
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WoS_20260204
dc.subjectNonlinear vibration
dc.subjectMultiple viscoelastic layers
dc.subjectFiber metal laminate plates
dc.subjectAmplitude dependence
dc.subjectPerk swerve phenomenon
dc.titleNonlinear vibration analysis of fiber metal laminated plates with multiple viscoelastic layers
dc.typeArticle

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