Abstract
The study focuses on the buckling analysis of laminated composite plates with different boundary conditions using a modified Fourier series. The analysis is based on classical laminated plate theory and employs the Rayleigh-Ritz method. The equation of motion for the plates is derived using the principle of virtual work and solved using a modified Fourier displacement function that satisfies general edge conditions. The eigenvalue problem generated by the Ritz method is solved using MATLAB for symmetric and anti-symmetric, cross and angle-ply laminated plates, considering design parameters such as aspect ratios, number of layers, lamination type, and orthotropic ratio. The results obtained show good agreement with those published by other researchers
Keywords
Buckling load
composite laminated plate
different edge conditions
Rayleigh-Ritz method