Modelling and Simulation in Engineering / 2012 / Article / Fig 5

Research Article

Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression

Figure 5

(a) Buckling shapes of a composite cylindrical panel with ply sequence of , which appear as the first buckling mode depending on the composite ply angle. (b) Variations of the first buckling load of composite cylindrical shell versus the composite ply angle.

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