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BUCKLING OF COMPOSITE PLATES SUBJECTED TO SHEAR AND LINERLY VARRYING LOADS

In this paper explicit expressions are developed for the calculation of the buckling loads of long, rectangular composite plates with orthotropic layup. These results can be used for the local buckling analysis of thin-walled fiber reinforced plastic beams. For linearly varying axial load the known results for hinged supports are corrected and new results are presented for built-in and constrained edges; for shear load new results are presented for constrained edges. The results are based on the Rayleigh-Ritz method.