A nonlinear problem of deflection of isotropic cylindrical panels fixed along all edges and
subject to transverse load was considered within the first-order shear deformation theory
(FSDT) and the classical shell theory (CST). An effect of the parameter of curvature on
bending and membrane components and resultants of transverse forces was analyzed. Par-
ticular attention was drawn to the fact that the bending components were accompanied by
transverse deformations, whereas for the membrane components, the panel was transversely
perfectly rigid. Resultants of transverse forces can be significantly larger than the bending
components. In failure criteria of laminated structures, only the bending transverse forces
are employed.
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