Improving the dynamic behavior of the plate under supersonic air flow by using nonlinear energy sink

In this paper, a nonlinear energy sink is used to improve the dynamic behavior of a square plate in supersonic flow. The plate is examined with different boundary conditions. The effect of changing the parameters and installation location of nonlinear energy sink on improving the dynamic behavior of the plate has been studied. The governing equations are first obtained using Von Karman's plate theory and piston theory, and then discretized using the Rayleigh-Ritz process. These equations are then solved using the fourth-order Runge-Kutta method. Time history curves, phase portraits, Poincare maps, and bifurcation diagrams were used to investigate the dynamic behavior and impact of nonlinear energy sink. The results show that the dynamic behavior of the plate is very complex in some cases, but with proper use of nonlinear energy sinks, this behavior can be improved.