The contribution of this work is the implementation of a new elastic solution method for thick laminated composites and sandwich structures based on a generalized unified formulation using finite elements. A quadrilateral four-node element was developed and evaluated using an in-house finite element program. The C-1 continuity requirements are fulfilled for the transversal displacement field variable. This method is tagged as Caliri's generalized formulation. The results employing the proposed solution method yielded coherent results with deviations as low as 0.05% for a static simply supported symmetric laminate and 0.5% for the modal analyses of a soft core sandwich structure. FINITE ELEMENT USING A GENERALIZED UNIFIED PLATE THEORY 291 the variety of theories developed to solve such complex laminated structures. When carefully analyzed, some of these theories can be grouped into the so-called unified or generalized theories.Li and Liu [9] exploited the concept of superposition and proposed a global-local refined multilayered plate theory. Such theory can be classified as an equivalent single layer (ESL) theory because the number of degrees of freedom was made independent of the number of layers through zig-zag refinements. However, despite its generalization, this formulation lacks unification properties. Unified plate/shell theories can group nearly all existing pate/shell theories into one from which they can be derived.In addition, when using unified formulations, theories with different orders of expansions can be directly compared, because no changes (but the index of the order of the thickness expansion) in the theory or solution method are performed to carry out the comparison. Moreover, other typing and precision errors, which may appear because of the use of different implemented solution methods, can be avoided. In addition, it is a powerful formulation to be implemented as a computer program. The works of Carrera, Demasi and Ferreira et al. [10][11][12][13][14][15][16][17][18][19][20][21][22][23] bring an extensive review and evaluation of the topic. Carrera [10,11] proposed a unification method, which generates a kernel matrix from which infinite axiomatic plate/shell theories can be extracted. Demasi improved Carrera's proposal and generalized it by decoupling the order of the displacement fields in each direction [14][15][16][17][18][19][20][21][22].Considering the aforementioned scope, this paper works on a new finite element solution method to solve thick laminates and sandwich elastic plates. The main contribution of this work is the implementation of a new solution approach, using the FEM, in order to solve unified plate formulations. The novelty of the present work is that the finite element solution is not fully C-0, but it now preserves the C-1 continuity requirements of the transverse displacement field. Carrera [10-13] also showed finite element results, along with closed-form solutions, but they are C-0 solutions. Thus, the present method (tagged as Caliri's generalized formulation -CGF)...