Single- vs Multilayer Plate Modelings on the Basis of Reissner's Mixed Theorem

The use of Reissner's mixed variational theorem (Reissner, E., On a Certain Mixed Variational Theory and a Proposed Applications, International Journal for Numerical Methods in Engineering, Vol. 20, 1984, pp. 1366-1368; Reissner, E.,On a Mixed Variational Theorem and on a Shear Deformable Plate Theory, International Journal of Numerical Methods in Engineering, Vol. 23, 1986, pp. 193-198) to analyze laminated plate structures is examined. The two cases of single-layer and multilayer models have been compared. Governing equilibrium and constitutive equations have been derived in a unified manner. Navier-type closed-form solutions are presented for the particular case of cross-ply simply supported plates. Thin and thick, as well as symmetrically and asymmetrically laminated plates, have been investigated. Displacements and transverse stresses have been evaluated and compared with available mixed two-dimensional results and three-dimensional solutions. The following have been concluded: 1) Reissner's mixed theorem is a very suitable tool to analyze laminated structures. 2) Multilayer modelings lead to an excellent agreement with exact solution for both displacement and transverse stress evaluations. Such an agreement, which has been confirmed for very thick geometries (a/h ≤ 4), does not depend on laminate layouts. No remarkable differences have been found for stresses evaluated a priori by the assumed model with respect to exact results. 3) Single-layer analyses lead to an accurate description of the response of thick plates. Major discrepancies have been found for very thick plate geometries with exact solutions. Nevertheless, their accuracy is very much subordinate to the order of the used expansion as well as to laminated layouts. Better transverse stress evaluations are obtained upon integration of three-dimensional equilibrium equations a posteriori than those furnished a priori. This trend has been confirmed for both thick and thin plates.

[1]  Koganti M. Rao,et al.  Analysis of thick laminated anisotropic composite plates by the finite element method , 1990 .

[2]  A. Toledano,et al.  SHEAR-DEFORMABLE TWO-LAYER PLATE THEORY WITH INTERLAYER SLIP , 1988 .

[3]  Erasmo Carrera,et al.  CZ° requirements—models for the two dimensional analysis of multilayered structures , 1997 .

[4]  Ahmed K. Noor,et al.  Stress and free vibration analyses of multilayered composite plates , 1989 .

[5]  Hidenori Murakami,et al.  A high-order laminated plate theory with improved in-plane responses☆ , 1987 .

[6]  E. Reissner On a mixed variational theorem and on shear deformable plate theory , 1986 .

[7]  E. Carrera An Improved Reissner-Mindlin-Type Model for the Electromechanical Analysis of Multilayered Plates Including Piezo-Layers , 1997 .

[8]  E. Carrera Developments, ideas, and evaluations based upon Reissner’s Mixed Variational Theorem in the modeling of multilayered plates and shells , 2001 .

[9]  E. Carrera A refined multilayered finite-element model applied to linear and non-linear analysis of sandwich plates , 1998 .

[10]  T. K. Varadan,et al.  Reissner’s New Mixed Variational Principle Applied to Laminated Cylindrical Shells , 1992 .

[11]  Hidenori Murakami,et al.  Laminated Composite Plate Theory With Improved In-Plane Responses , 1986 .

[12]  E. Carrera,et al.  An investigation of non-linear dynamics of multilayered plates accounting for C0z requirements , 1998 .

[13]  Erasmo Carrera,et al.  Multilayered Shell Theories Accounting for Layerwise Mixed Description, Part 1: Governing Equations , 1999 .

[14]  Erasmo Carrera,et al.  Evaluation of Layerwise Mixed Theories for Laminated Plates Analysis , 1998 .

[15]  J. Reddy Mechanics of laminated composite plates : theory and analysis , 1997 .

[16]  E. Reissner,et al.  Reflections on the Theory of Elastic Plates , 1985 .

[17]  E. Carrera,et al.  An evaluation of geometrical nonlinear effects of thin and moderately thick multilayered composite shells , 1997 .

[18]  A. M. Waas,et al.  Analysis of a rotating multi-layer annular plate modeled via layerwise zig-zag theory: Free vibration and transient analysis , 1998 .

[19]  E. Carrera A Reissner’s Mixed Variational Theorem Applied to Vibration Analysis of Multilayered Shell , 1999 .

[20]  Maenghyo Cho,et al.  Efficient higher order composite plate theory for general lamination configurations , 1993 .

[21]  E. Reissner On a certain mixed variational theorem and a proposed application , 1984 .

[22]  E. Carrera Layer-Wise Mixed Models for Accurate Vibrations Analysis of Multilayered Plates , 1998 .

[23]  C. Sun,et al.  Theories for the Dynamic Response of Laminated Plates , 1973 .

[24]  E. Carrera,et al.  Zig-Zag and interlaminar equilibria effects in large deflection and postbuckling analysis of multilayered plates , 1997 .

[25]  E. Carrera C0 REISSNER–MINDLIN MULTILAYERED PLATE ELEMENTS INCLUDING ZIG-ZAG AND INTERLAMINAR STRESS CONTINUITY , 1996 .

[26]  Hung-Sying Jing,et al.  Refined shear deformation theory of laminated shells , 1993 .

[27]  N. Pagano,et al.  Exact Solutions for Composite Laminates in Cylindrical Bending , 1969 .

[28]  T. K. Varadan,et al.  A higher-order theory for bending analysis of laminated shells of revolution , 1991 .

[29]  N. J. Pagano,et al.  Elastic Behavior of Multilayered Bidirectional Composites , 1972 .

[30]  Erasmo Carrera,et al.  Multilayered Shell Theories Accounting for Layerwise Mixed Description, Part 2: Numerical Evaluations , 1999 .

[31]  Hidenori Murakami,et al.  A Composite Plate Theory for Arbitrary Laminate Configurations. , 1987 .