On the prediction improvement of transverse stress distributions in cross-ply laminated beams: advanced versus conventional beam modelling

Abstract This paper assesses the stress analysis performance of the most commonly used conventional, shear deformable beam theories as well as the advanced beam theories presented in references [Acta Mech. 1997;123:163; Math. Mech. Solids 1997;2:459; Int. J. Solids Struct. 1997;22:2857], by employing a predictor–corrector method. The assessment deals with the accuracy of the distribution of the interlaminar (transverse shear and transverse normal) stresses through the entire beam thickness. As far as simply supported, cross-ply laminated beams are concerned, it compares the corresponding stress analysis results obtained with their exact elasticity counterparts. The conclusions of this type of initial assessment are very much in favour of the advanced beam theories, which involve exponential shape functions of the transverse co-ordinate parameter. Hence, those advanced beam theories are employed for further applications that involve different sets of end boundary conditions for which explicit exact elasticity results are unavailable or very difficult to obtain.

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

[2]  Rudolf Heuer,et al.  Static and dynamic analysis of transversely isotropic, moderately thick sandwich beams by analogy , 1992 .

[3]  Xiaoping Shu,et al.  Cylindrical bending of angle-ply laminates subjected to different sets of edge boundary conditions , 2000 .

[4]  J. Whitney,et al.  Shear Correction Factors for Orthotropic Laminates Under Static Load , 1973 .

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

[6]  A. Noor,et al.  Accurate determination of transverse normal stresses in sandwich panels subjected to thermomechanical loadings , 1999 .

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

[8]  K. C. Jane,et al.  Interlaminar stresses of a rectangular laminated plate with simply supported edges subject to free vibration , 2000 .

[9]  T. Chow,et al.  On the Propagation of Flexural Waves in an Orthotropic Laminated Plate and Its Response to an Impulsive Load , 1971 .

[10]  G. Cowper The Shear Coefficient in Timoshenko’s Beam Theory , 1966 .

[11]  L. Librescu,et al.  Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings , 1996 .

[12]  Julio F. Davalos,et al.  Static shear correction factor for laminated rectangular beams , 1996 .

[13]  L. Librescu,et al.  Comprehensive Model of Anisotropic Composite Aircraft Wings Suitable for Aeroelastic Analyses , 1994 .

[14]  Shulong Liu,et al.  On “The generalised plane strain deformations of thick anisotropic composite laminated plates” , 2001 .

[15]  J. M. Whitney,et al.  Dynamic Response of Laminated Composite Plates , 1975 .

[16]  M. D. Sciuva,et al.  BENDING, VIBRATION AND BUCKLING OF SIMPLY SUPPORTED THICK MULTILAYERED ORTHOTROPIC PLATES: AN EVALUATION OF A NEW DISPLACEMENT MODEL , 1986 .

[17]  Kostas P. Soldatos,et al.  A method for improving the stress analysis performance of one- and two-dimensional theories for laminated composites , 1997 .

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

[19]  K. Soldatos,et al.  A general theory for the accurate stress analysis of homogeneous and laminated composite beams , 1997 .

[20]  T. K. Varadan,et al.  Free vibration and stability of cross-ply laminated plates , 1990 .

[21]  S. Vel,et al.  The generalized plane strain deformations of thick anisotropic composite laminated plates , 2000 .

[22]  K. Soldatos,et al.  Accurate Stress Analysis of Laminated Plates Combining a Two-Dimensional Theory with the Exact Three-Dimensional Solution for Simply Supported Edges , 1997 .