Accuracy of critical-temperature sensitivity coefficients predicted by multilayered composite plate theories

An assessment is made of the accuracy of the critical-temperature sensitivity coefficients of multilayered plates predicted by different modeling approaches, based on two-dimensional shear-deformation theories. The sensitivity coefficients considered measure the sensitivity of the critical temperatures to variations in different lamination and material parameters of the plate. The standard of comparison is taken to be the sensitivity coefficients obtained by the three-dimensional theory of thermoelasticity. Numerical studies are presented showing the effects of variation in the geometric and lamination parameters of the plate on the accuracy of both the sensitivity coefficients and the critical temperatures predicted by the different modeling approaches.

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

[2]  Chang Jeng-Shian FEM analysis of buckling and thermal buckling of antisymmetric angle-ply laminates according to transverse shear and normal deformable high order displacement theory , 1990 .

[3]  Y. Stavsky Thermoelastic stability of laminated orthotropic circular plates , 1975 .

[4]  T. R. Tauchert THERMAL BUCKLING OF THICK ANTISYMMETRIC ANGLE-PLY LAMINATES , 1987 .

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

[6]  T. Hsu,et al.  Thermal buckling of laminated composite plates with transverse shear deformation , 1990 .

[7]  James M. Whitney,et al.  Effect of Environment on the Elastic Response of Layered Composite Plates , 1971 .

[8]  Ahmed K. Noor,et al.  Stiffness and thermoelastic coefficients for composite laminates , 1992 .

[9]  Ahmed K. Noor,et al.  Three-dimensional solutions for thermal buckling of multilayered anisotropic plates , 1992 .

[10]  Strain energy of thermally stressed multilayer panels and its sensitivity coefficients , 1993 .

[11]  T. R. Tauchert,et al.  Thermal Buckling of Symmetric Angle-ply Laminated Plates , 1987 .

[12]  E. J. Brunelle,et al.  Thermal Buckling of Initially Stressed Thick Plates , 1981 .

[14]  A. Cemal Eringen CHAPTER VIII – Three-Dimensional Solutions , 1975 .

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

[16]  S. Srinivas,et al.  A refined analysis of composite laminates , 1973 .

[17]  Ahmed K. Noor,et al.  Predictor-corrector procedures for thermal buckling analysis of multilayered composite plates , 1991 .

[18]  J. Ramachandran,et al.  Thermal buckling of composite laminated plates , 1989 .

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

[20]  A. Noor,et al.  Thermomechanical Buckling of Multilayered Composite Plates , 1992 .