Assessment of the refined sinus model for the non-linear analysis of composite beams

The objective of this paper is to evaluate a new three-noded mechanical beam finite element for the non-linear analysis of laminated beams. It is based on a sinus distribution with layer refinement. The transverse shear strain is obtained by using a cosine function avoid-ing the use of shear correction factors. This kinematic accounts for the interlaminar continuity conditions on the interfaces between lay-ers, and the boundary conditions on the upper and lower surfaces of the beam. A conforming FE approach is carried out using Lagrange and Hermite interpolations. It is important to notice that the number of unknowns is independent from the number of layers. Buckling, post-buckling, and non-linear bending tests are presented in order to compare with the ones available in the literature or based on a 2D analysis. The influence of mesh, boundary conditions, length-to-thickness ratios and lay-ups is studied to show the accu-racy and the efficiency of this finite element.

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

[2]  Anthony M. Waas,et al.  Effects of shear deformation on buckling and free vibration of laminated composite beams , 1997 .

[3]  P. Subramanian,et al.  Dynamic analysis of laminated composite beams using higher order theories and finite elements , 2006 .

[4]  Hiroyuki Matsunaga,et al.  Interlaminar stress analysis of laminated composite beams according to global higher-order deformation theories , 2002 .

[5]  Tarun Kant,et al.  On the performance of higher order theories for transient dynamic analysis of sandwich and composite beams , 1997 .

[6]  Maurice Touratier,et al.  A generalization of shear deformation theories for axisymmetric multilayered shells , 1992 .

[7]  Dahsin Liu,et al.  GENERALIZED LAMINATE THEORIES BASED ON DOUBLE SUPERPOSITION HYPOTHESIS , 1997 .

[8]  H. Murakami,et al.  TRANSIENT THERMAL STRESS ANALYSIS OF A LAMINATED COMPOSITE BEAM , 1989 .

[9]  K. Chandrashekhara,et al.  Linear and geometrically non-linear analysis of composite beams under transverse loading , 1993 .

[10]  E. Carrera Historical review of Zig-Zag theories for multilayered plates and shells , 2003 .

[11]  K. Y. Sze,et al.  Finite element model with continuous transverse shear stress for composite laminates in cylindrical bending , 1998 .

[12]  Ugo Icardi,et al.  Higher-order zig-zag model for analysis of thick composite beams with inclusion of transverse normal stress and sublaminates approximations , 2001 .

[13]  Kostas P. Soldatos,et al.  On the prediction improvement of transverse stress distributions in cross-ply laminated beams: advanced versus conventional beam modelling , 2002 .

[14]  Metin Aydogdu,et al.  Buckling analysis of cross-ply laminated beams with general boundary conditions by Ritz method , 2006 .

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

[16]  Dahsin Liu,et al.  Static and vibration analysis of laminated composite beams with an interlaminar shear stress continuity theory , 1992 .

[17]  J. N. Reddy,et al.  On refined computational models of composite laminates , 1989 .

[18]  I. Elishakoff,et al.  A transverse shear and normal deformable orthotropic beam theory , 1992 .

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

[20]  M. Karama,et al.  Bending, buckling and free vibration of laminated composite with a transverse shear stress continuity model , 1998 .

[21]  Philippe Vidal,et al.  A thermomechanical finite element for the analysis of rectangular laminated beams , 2006 .

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

[23]  M. Touratier,et al.  An efficient standard plate theory , 1991 .

[24]  Olivier Polit,et al.  A new eight‐node quadrilateral shear‐bending plate finite element , 1994 .

[25]  Rakesh K. Kapania,et al.  Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling. , 1989 .

[26]  Ronald C. Averill,et al.  An improved theory and finite-element model for laminated composite and sandwich beams using first-order zig-zag sublaminate approximations , 1997 .

[27]  J. N. Reddy,et al.  A generalization of two-dimensional theories of laminated composite plates† , 1987 .

[28]  Srinivasan Gopalakrishnan,et al.  A refined higher order finite element for asymmetric composite beams , 2005 .

[29]  E. Carrera Theories and finite elements for multilayered, anisotropic, composite plates and shells , 2002 .

[30]  Hiroyuki Matsunaga,et al.  VIBRATION AND BUCKLING OF MULTILAYERED COMPOSITE BEAMS ACCORDING TO HIGHER ORDER DEFORMATION THEORIES , 2001 .

[31]  Ahmed A. Khdeir,et al.  Buckling of cross-ply laminated beams with arbitrary boundary conditions , 1997 .

[32]  Olivier Polit,et al.  High-order triangular sandwich plate finite element for linear and non-linear analyses , 2000 .

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

[34]  Sébastien Mistou,et al.  Mechanical behaviour of laminated composite beam by the new multi-layered laminated composite structures model with transverse shear stress continuity , 2003 .

[35]  K. Chandrashekhara,et al.  Some observations on the modeling of laminated composite beams with general lay-ups , 1991 .

[36]  C. M. Mota Scares,et al.  Buckling behaviour of laminated beam structures using a higher-order discrete model , 1997 .

[37]  Raimund Rolfes,et al.  A three-layered sandwich element with improved transverse shear stiffness and stresses based on FSDT , 2006 .

[38]  E. Carrera On the use of the Murakami's zig-zag function in the modeling of layered plates and shells , 2004 .

[39]  J. Reddy Mechanics of laminated composite plates and shells : theory and analysis , 1996 .

[40]  Gangan Prathap,et al.  Beam elements based on a higher order theory—I. Formulation and analysis of performance , 1996 .

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

[42]  Olivier Polit,et al.  A family of sinus finite elements for the analysis of rectangular laminated beams , 2008 .

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

[44]  Ugo Icardi,et al.  Numerical assessment of the core deformability effect on the behavior of sandwich beams , 1999 .

[45]  Maurice Touratier,et al.  A refined theory of laminated shallow shells , 1992 .

[46]  Santosh Kapuria,et al.  Assessment of zigzag theory for static loading, buckling, free and forced response of composite and sandwich beams , 2004 .

[47]  Olivier Polit,et al.  AC1 finite element including transverse shear and torsion warping for rectangular sandwich beams , 1999 .

[48]  Olivier Polit,et al.  C1 plate and shell finite elements for geometrically nonlinear analysis of multilayered structures , 2006 .

[49]  Zhen Wu,et al.  Refined laminated composite plate element based on global–local higher-order shear deformation theory , 2005 .

[50]  Ronald C. Averill,et al.  Development of simple, robust finite elements based on refined theories for thick laminated beams , 1996 .