International Journal of Aerospace Engineering / 2015 / Article / Fig 2

Research Article

Nonlinear Vibrations of FGM Cylindrical Panel with Simply Supported Edges in Air Flow

Figure 2

Comparison of nondimensional center deflection of the square plate with simply supported edges under a suddenly applied uniform load by Reddy’s FEM results [29] and present (—: present; ■: Reddy’s).