Nonlinear dynamic responses of CNT-reinforced panels with complex curvature, piezoelectric layer, and CNT-reinforced stiffeners.

In this paper, the nonlinear vibration and dynamic buckling responses of the sinusoid, parabola, and cylindrical CNT-reinforced panels with piezoelectric layer stiffened by a CNT-reinforced stiffener system in uniform temperature change with a piezoelectric layer are presented. An improved homogenization technique for the x - or y -direction CNT-reinforced stiffener system is utilized to determine the total stiffnesses of the considered structures. The higher-order shear deformation theory (HSDT) in conjunction with the von Kármán nonlinearities is adopted to formulate the motion equations, while the stress function for complex curvature panels is estimated using the like-Galerkin procedure. The nonlinear equation of motion is acquired by utilizing the Lagrange function and Euler-Lagrange's equations. The numerical examples use the Runge-Kutta technique to acquire the nonlinear time-amplitude curves, and the critical dynamic buckling load is determined using the Budiansky-Roth criterion. These examples evaluate the effects of stiffeners, piezoelectric layer, material, and geometrical parameters on the nonlinear vibration and dynamic buckling responses of the panels. • Nonlinear dynamic responses of the CNT-reinforced stiffened panels are studied. • Sinusoid, parabola, and cylindrical panels with piezoelectric layer are mentioned. • The improved smeared stiffener technique for CNT-reinforced stiffeners is presented. • The like-Galerkin procedure is applied to estimate the approximate stress function. • HSDT, Euler-Lagrange's equation, and Runger-Kutta method are used. [ABSTRACT FROM AUTHOR]