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

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</svg>, 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.</table>

Modelling and Simulation in Engineering

fig5

Figure 5

Figure 5: Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression 