Abstract

Nonlinear free vibration responses of functionally graded single/doubly curved shell panels are computed based on higher order shear deformation theory and Green-Lagrange type nonlinearity. The material properties of functionally graded materials are obtained based on the Voigt model in conjunction with power-law distribution for a smooth variation of material along with the thickness coordinate. The governing equation of the vibrated curved panel has been obtained using Hamilton’s principle. The model has been discretized using a nine node quadrilateral Lagrangian shell element and solved numerically using a direct iterative method. The convergence and comparison behavior of the nonlinear model has been checked by comparing the responses with the published literature. The influence of the power-law index, curvature ratio, thickness ratio, aspect ratio, amplitude ratio and support conditions on the nonlinear responses of cylindrical, elliptical and hyperbolic shell panels are discussed.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call