Abstract
In the present investigation, buckling of functionally graded carbon nanotube reinforced composite (FGCNTRC) plate with a cutout is studied by the finite element method. The formulation based on a higher-order shear deformation theory. An eight noded isoparametric plate bending element with nine degrees of freedom at each node is used. The critical loads for various volume fractions and CNT patterns are presented for simply supported boundary condition.In the present investigation, buckling of functionally graded carbon nanotube reinforced composite (FGCNTRC) plate with a cutout is studied by the finite element method. The formulation based on a higher-order shear deformation theory. An eight noded isoparametric plate bending element with nine degrees of freedom at each node is used. The critical loads for various volume fractions and CNT patterns are presented for simply supported boundary condition.
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