International Journal of Aerospace Engineering / 2015 / Article / Fig 5

Research Article

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

Figure 5

The multiple-periodic motion of the FGM cylindrical panel occurs when the magnitude of the in-plane excitation is taken to be . The volume fraction index is taken to be 0.5. The Mach number is taken to be 5.0.
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