Abstract

The effect of hygrothermal conditions on the buckling and postbuckling of shear deformable laminated cylindrical panels subjected to axial compression is investigated using a micro-to-macro-mechanical analytical model. The material properties of the composite are affected by the variation of temperature and moisture, and are based on a micro-mechanical model of a laminate. The governing equations are based on Reddy's higher order shear deformation shell theory with von Kármán–Donnell-type of kinematic nonlinearity and including hygrothermal effects. The nonlinear prebuckling deformations and initial geometric imperfections of the panel are both taken into account. A boundary layer theory of shell buckling is extended to the case of shear deformable laminated cylindrical panels under hygrothermal environments and a singular perturbation technique is employed to determine the buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling behavior of perfect and imperfect, moderately thick and thin, cross-ply laminated cylindrical panels under different sets of environmental conditions. The results show that the hygrothermal environment has a significant effect on the buckling load as well as postbuckling response of the panel. In contrast, it has a small effect on the imperfection sensitivity of symmetric cross-ply laminated cylindrical thin panels.

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