This study presents an assessment of classical lamination shell theory and first-order shear deformation theory for a simply supported finite circular cylindrical hybrid shell with a cross-ply laminate as an elastic substrate under thermoelectric static load. Navier-type solutions for these shell theories are obtained and used in three-dimensional (3D)equilibrium equations and transverse strain-displacement relations to obtain transverse stress components and an improved value of deflection. These solutions are assessed by comparison with the 3D solution.
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Kapuria et al. (1998) studied this question.
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