Reddy's layerwise theory is used to perform free-vibration analysis of
laminated plates. This theory is the most current and sophisticated t
heory in which full account is given to various three-dimensional effe
cts. The results obtained from this theory are compared with those obt
ained from a full-fledged three-dimensional elasticity analysis and va
rious equivalent single-layer theories that are available. These inclu
de the classical laminated plate theory (CLPT), the first-order shear
deformation laminated plate theory (FSDPT), and the third-order shear
deformation plate theory (THSDPT). The elasticity equations are solved
by utilizing the state-space variables and the transfer matrix. A det
ailed analysis is carried out, by uncoupling the Navier equations, to
study the various mode shapes and natural frequencies of a homogeneous
transversely isotropic plate. Results are also obtained for symmetric
and antisymmetric cross-ply laminates.