A combined numerical-and-analytical technique for studying the geometrically nonlinear vibrations of thin shells of revolution with piezoelectric layers is proposed. The technique uses the finite-element method and the method of harmonic linearization. The results of numerical modeling of a cylindrical panel having similar piezoelectric face layers and a passive viscoelastic core layer are presented. The behavior of the deflection in the vicinity of the first resonance at various damping coefficients is studied in detail.
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Translated from Prikladnaya Mekhanika, Vol. 57, No. 2, pp. 88–106, March–April 2021.
* This study was sponsored by the budget program “Support for Priority Areas of Scientific Research” (KPKVK 6541230).
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Kozlov, V.I., Zinchuk, L.P., Karnaukhova, T.V. et al. Forced Geometrically Nonlinear Vibrations of Thin Shells of Revolution with Piezoelectric Layers*. Int Appl Mech 57, 200–216 (2021). https://doi.org/10.1007/s10778-021-01074-6
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DOI: https://doi.org/10.1007/s10778-021-01074-6