Higher-order theories for thermal stresses in layered plates

First order shear deformation theory renders quite accurate in-plane stresses even for rather thick plates. By means of equilibrium conditions derivatives of the in-plane stresses can be integrated to determine transverse shear and normal stresses. The need to use in-plane derivatives requires at least cubic shape functions. Simplifying assumptions relieve these requirements leading to the extended 2D method. While under mechanical load this method yields excellent results, poor transverse normal stresses have been obtained for plates under a sinusoidal temperature distribution. This paper traces back these deficiencies to lentil-like deformations of each separate layer. It is proved that third or fifth order displacement approximations through the plate thickness avoid these deficiencies.

[1]  J. Whitney,et al.  Shear Deformation in Heterogeneous Anisotropic Plates , 1970 .

[2]  Raimund Rolfes,et al.  Efficient linear transverse normal stress analysis of layered composite plates , 1998 .

[3]  O. Orringer,et al.  Alternate Hybrid-Stress Elements for Analysis of Multilayer Composite Plates , 1977 .

[4]  Charles W. Bert,et al.  Three-dimensional elasticity solutions for free vibrations of rectangular plates by the differential quadrature method , 1998 .

[5]  J. N. Reddy,et al.  Modelling of thick composites using a layerwise laminate theory , 1993 .

[6]  Werner Wagner,et al.  On the numerical analysis of local effects in composite structures , 1994 .

[7]  N. Pagano,et al.  Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates , 1970 .

[8]  J. E. Akin,et al.  Analysis of layered composite plates using a high-order deformation theory , 1987 .

[9]  Ahmed K. Noor,et al.  Three-dimensional solutions for antisymmetrically laminated anisotropic plates , 1990 .

[10]  R. Christensen,et al.  A High-Order Theory of Plate Deformation—Part 2: Laminated Plates , 1977 .

[11]  David R. Owen,et al.  A refined analysis of laminated plates by finite element displacement methods—I. Fundamentals and static analysis , 1987 .

[12]  K. Rohwer,et al.  Application of higher order theories to the bending analysis of layered composite plates , 1992 .

[13]  Thermal buckling analysis of antisymmetric angle-ply laminates based on a higher-order displacement field , 1991 .

[14]  S. Vel,et al.  Analytical Solution for Rectangular Thick Laminated Plates Subjected to Arbitrary Boundary Conditions , 1999 .

[15]  Raimund Rolfes,et al.  Calculating 3D stresses in layered composite plates and shells , 1998 .

[16]  Reaz A. Chaudhuri,et al.  An equilibrium method for prediction of transverse shear stresses in a thick laminated plate , 1986 .

[17]  Robert L. Spilker,et al.  Hybrid-stress eight-node elements for thin and thick multilayer laminated plates , 1982 .

[18]  Raimund Rolfes,et al.  Improved transverse shear stresses in composite finite elements based on first order shear deformation theory , 1997 .

[19]  Tarun Kant,et al.  Flexural analysis of laminated composites using refined higher-order C ° plate bending elements , 1988 .

[20]  Ahmed K. Noor,et al.  Evaluation of Transverse Thermal Stresses in Composite Plates Based on First-Order Shear Deformation Theory , 1998 .

[21]  Ahmed K. Noor,et al.  Predictor-corrector procedures for stress and free vibration analysis of multilayered composite plates and shells , 1990 .

[22]  P. Tong,et al.  Finite Element Solutions for Laminated Thick Plates , 1972 .

[23]  A. K. Noor,et al.  An assessment of five modeling approaches for thermo-mechanical stress analysis of laminated composite panels , 2000 .

[24]  A. Rao,et al.  Bending, vibration and buckling of simply supported thick orthotropic rectangular plates and laminates , 1970 .

[25]  J. Reddy,et al.  Thermal stresses and deflections of cross-ply laminated plates using refined plate theories , 1991 .

[26]  J. Reddy A Simple Higher-Order Theory for Laminated Composite Plates , 1984 .