Mixed plate theories based on the Generalized Unified Formulation.: Part II: Layerwise theories
Introduction
Equivalent single layer theories give a sufficiently accurate description of the global laminate response. However, these theories are not adequate for determining the stress fields at ply level. Layerwise theories assume separate displacement field expansions within each layer. The accuracy is then greater but the price is in the increased computational cost. Many layerwise plate models have been proposed in the past by applying classical plate theory or higher order theories at each layer. Generalizations of these approaches were also given, and the displacements variables were expressed in terms of Lagrange polynomials. Among the papers devoted on the subject of layerwise theories, Refs. [1], [2], [3], [4], [5] give an idea of the different approaches. Normally, displacement-based layerwise models do not a priori take into account the continuity of the transverse stresses between two adjacent layers. The problem of satisfying the interlaminar continuity of the transverse stresses a priori led to the derivation of mixed layerwise theories [6], [7], [8]. Layerwise theories could also be easily extended to the case of composite beams as explained in Ref. [9]. The conceptual differences between the displacement fields in layerwise and equivalent single layer theories are depicted in Fig. 1. Layerwise models are computationally more expensive than the less accurate equivalent single layer models. Therefore, layerwise models can be used in regions of the structure in which an accurate description is required [10], whereas equivalent single layer models are employed in other parts of the structure. It is also possible to develop quasi-layerwise theories in which some quantities are described using the layerwise approach and some are described using the equivalent single layer approach. These two categories of theories will be described in Part III Ref. [11] and Part IV Ref. [12] of this work.
The generalized unified formulation (GUF) [13], [14] is a new formalism and a generalization of Carrera’s Unified Formulation (CUF) [15]. GUF was introduced in the case of displacement-based theories. GUF was extended, for the first time in the literature, to the case of mixed theories (see Part I, Ref. [16]). In particular, Reissner’s mixed variational theorem (RMVT) (see [17], [18]) was employed. The unknown variables were the displacements and transverse stresses.
In the present work GUF will be extended to the case of composite multilayered structures analyzed with layerwise models. Each layer variable (a displacement or a transverse stress) will be independently expanded along the thickness leading to a very wide variety of new theories. Since each variable can be expanded in infinite different forms (by simply changing the order of the polynomial used in the expansion along the thickness), the case of RMVT-based theories leads to the writing of layerwise mixed theories. All the possible theories generated using GUF can be implemented in a single code without the requirements of new implementations or theoretical developments.
This is a new powerful methodology to create layerwise theories, and the details will be given in this work. In particular, it will be shown how to generate the layer matrices from the fundamental nuclei or kernels (introduced in Part I, Ref. [16]) and how to assemble these matrices. The interlaminar continuity of the displacements and transverse stresses is taken into account. Numerous examples clarify how to use GUF to generate a desired layerwise theory.
Section snippets
Theoretical derivation of layerwise mixed theories
For a generic layer k, the displacements , , and out-of-plane stresses , , are written in a compact notation (the generalized unified formulation) as follows:
Kernels of the generalized unified formulation
In Part I Ref. [16] the governing equations (Navier-type solution) were written with a Compact Notation: the generalized unified formulation. All of the equations, including different combinations, were written as function of kernels of the generalized unified formulation. In particular, six pressure kernels of matrices were introduced. Also, 21 kernels were used to generate the matrices (but only 13 are really required). The fundamental equations, invariant with respect to the orders
Theoretical examples
The generation of the infinite theories is not a very difficult problem when the generalized unified formulation is used. To help the readers create their own code based on this procedure, the author reports here several numerical examples. In particular, theory will be analyzed in detail. Suppose that the goal is the generation of matrix .
The kernel associated with matrix (at layer level) is the following:
Calculation of the stresses
The system of equations with unknown amplitudes of displacements and stresses is represented by Eq. (17). This system can either be directly solved or the static condensation technique (see part I, Ref. [16]) can be performed. When the Navier-type solution is considered it is not really important if the static condensation is performed or not, but when FEM computations are concerned, the static condensation (if performed at element level) can significantly save CPU time. Suppose now the
Conclusion
For the first time in the literature, the extension of the generalized unified formulation to the cases of mixed variational statements (in particular Reissner’s mixed variational theorem) and layerwise theories is presented. The displacements , , and the stresses , , are expanded along the thickness of each layer by using Legendre polynomials. Each variable can be treated separately from the others. This allows the writing, with a single formal derivation and software,
Acknowledgement
The author thanks his sister Demasi Paola who inspired him with her strong will.
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