International Journal of Aerospace Engineering / 2015 / Article / Fig 7

Research Article

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

Figure 7

(a) and (b) depict the bifurcation diagrams of versus and which are given when the Mach number is taken to be 10.0. The value of horizontal coordinate has the same definition as that in Figure 3.
(a)
(b)