Abstract
Free boundary and interfacial vibrations of a composite cylindrical panel with free edges comprised of two finite orthotropic thin cylindrical panels with different elastic properties and full contact along the generators are studied. Starting from the formulation of the classical theory of orthotropic cylindrical shells, dispersion relations and asymptotic approximations for eigenfrequencies of interfacial and boundary vibrations of such composite cylindrical panels are derived. An algorithm for separating the interfacial and boundary vibrations is presented. Asymptotic connections between the dispersion relations of the problem at hand and the analogous problems for a composite rectangular plate are established. Examples of cylindrical panel with different widths of constituents are considered, and approximate values of dimensionless eigenfrequencies are obtained.
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Ghulghazaryan, G., Ghulghazaryan, L. (2023). Free Localized Vibrations of a Thin Elastic Composite Panel. In: Altenbach, H., Prikazchikov, D., Nobili, A. (eds) Mechanics of High-Contrast Elastic Solids. Advanced Structured Materials, vol 187. Springer, Cham. https://doi.org/10.1007/978-3-031-24141-3_7
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