A higher order displacement based formulation has been developed to investi
gate wave propagation in fiber-reinforced polymer composite laminated (FRPC
L) plates. The formulation has been applied, as an illustration, to a plate
made up of transversely isotropic laminae with the axes of symmetry lying
in the plane of the lamina. Results for the plane as well as the antiplane
strain cases are shown to be in excellent agreement with the exact solution
s for isotropic and transversely isotropic single layered plates. Also, num
erical results have been obtained for crossply (0 deg/90 deg/0 deg/90 deg)
laminated composite plates, which agree very well with the previously publi
shed numerical results. The formulation can be employed to expeditiously in
vestigate the dispersion characteristics of waves propagating in a plate wi
th an arbitrary number of anisotropic laminae.