Multilayered Shell Theories Accounting for Layerwise Mixed Description, Part 1: Governing Equations

A Reissner mixed variational equation is employed in this paper to derive the differential governing equations of multilayered, double curved shells made of orthotropic laminae In linear static cases. A layerwise description is referred to by assuming two independent fields in the thickness direction for the transverse stress (both shear and normal components) and displacement variables in each layer. Interlaminar values are used as the unknown variables of the introduced expansions. The continuity conditions of displacements and transverse shear and normals stresses at the interfaces between two consecutive layers, referred to as C 0 z requirements, have been a priori fulfilled. These have been used to drive the governing equations from a layer to a multilayered level. Classical displacement formulations and related equivalent single-layer equations have been derived for comparison purposes. No assumptions have been made concerning the terms of type thickness to radii shell ratio h/R. Donnell's shallow shell-type equations are given as particular cases for all of the considered theories. Indicial notations and arrays have been used extensively to handle the presented developments in a concise manner. Numerical evaluations and comparisons to exact and other available two-dimensional solutions are given in a companion paper (E. Carrera, Multilayered Shell Theories Accounting for Layerwise Mixed Description, Part 2: Numerical Evaluations, AIAA Journal, Vol. 37, No. 9, 1999, pp. 1117-1124).

[1]  V. Berdichevsky,et al.  Effect of Accuracy Loss in Classical Shell Theory , 1992 .

[2]  George Z. Voyiadjis,et al.  A Refined two-dimensional theory for thick cylindrical shells , 1991 .

[3]  Erasmo Carrera,et al.  Mixed layer-wise models for multilayered plates analysis , 1998 .

[4]  Teh-Min Hsu,et al.  A theory of laminated cylindrical shells consisting of layers of orthotropic laminae , 1970 .

[5]  I. P. Smirnov,et al.  Optimal control of a dynamic system with random parameters under incomplete information , 1979 .

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

[7]  A. Kalnins,et al.  Thin elastic shells , 1967 .

[8]  O. C. Holister,et al.  Stress Analysis , 1965 .

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

[10]  Erasmo Carrera,et al.  Elastodynamic Behavior of Relatively Thick, Symmetrically Laminated, Anisotropic Circular Cylindrical Shells , 1992 .

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

[12]  J. L. Sanders,et al.  Theory of thin elastic shells , 1982 .

[13]  Ekkehard Ramm,et al.  Hybrid stress formulation for higher-order theory of laminated shell analysis , 1993 .

[14]  Liviu Librescu,et al.  A shear deformable theory of laminated composite shallow shell-type panels and their response analysis I: Free vibration and buckling , 1989 .

[15]  T. K. Varadan,et al.  Bending of laminated orthotropic cylindrical shells—An elasticity approach , 1991 .

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

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

[18]  A. Noor,et al.  Assessment of Computational Models for Multilayered Composite Shells , 1990 .

[19]  Anthony N. Palazotto,et al.  Transverse shear deformation in orthotropic cylindrical pressure vessels using a higher-order shear theory , 1989 .

[20]  Y. C. Das,et al.  Vibration of layered shells , 1973 .

[21]  E. Carrera The effects of shear deformation and curvature on buckling and vibrations of cross-ply laminated composite shells , 1991 .

[22]  Liviu Librescu,et al.  Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures , 1975 .

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

[24]  W. Flügge Stresses in Shells , 1960 .

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

[26]  J. Ren,et al.  Exact solutions for laminated cylindrical shells in cylindrical bending , 1987 .

[27]  J. N. Reddy,et al.  A higher-order shear deformation theory of laminated elastic shells , 1985 .

[28]  A. L. Gol'denveizer Derivation of an approximate theory of shells by means of asymptotic integration of the equations of the theory of elasticity , 1963 .

[29]  J. Whitney,et al.  A Refined Theory for Laminated Anisotropic, Cylindrical Shells , 1974 .

[30]  Ahmed K. Noor,et al.  A posteriori estimates for shear correction factors in multilayered composite cylinders , 1989 .

[31]  K. Soldatos,et al.  A comparison of some shell theories used for the dynamic analysis of cross-ply laminated circular cylindrical panels , 1984 .

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

[33]  Rakesh K. Kapania,et al.  A Review on the Analysis of Laminated Shells Virginia Polytechnic Institute and State University , 1989 .

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

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

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

[37]  Ahmed K. Noor,et al.  Three-dimensional solutions of laminated cylinders , 1974 .

[38]  Erasmo Carrera,et al.  Multilayered shell finite element with interlaminar continuous shear stresses : a refinement of the Reissner-Mindlin formulation , 2000 .

[39]  J. Radok,et al.  The theory of thin shells , 1959 .

[40]  Ahmed K. Noor,et al.  Stress, vibration, and buckling of multilayered cylinders , 1989 .

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

[42]  Free vibrations of thick, layered cylinders having finite length with various boundary conditions , 1972 .

[43]  J. N. Reddy,et al.  General two-dimensional theory of laminated cylindrical shells , 1990 .

[44]  Liviu Librescu,et al.  A shear deformable theory of laminated composite shallow shell-type panels and their response analysis II: Static response , 1989 .

[45]  Erasmo Carrera,et al.  Single- vs Multilayer Plate Modelings on the Basis of Reissner's Mixed Theorem , 2000 .

[46]  Anthony N. Palazotto,et al.  Laminated shell in cylindrical bending, two-dimensional approach vs exact , 1991 .