“…Moreover, it is known that Ritz method is efficient to deal with composite and FG beams with arbitrary boundary conditions. The accuracy and efficiency of this approach can be found in some representative earlier works [24,26,[40][41][42][43][44].…”
“…Moreover, it is known that Ritz method is efficient to deal with composite and FG beams with arbitrary boundary conditions. The accuracy and efficiency of this approach can be found in some representative earlier works [24,26,[40][41][42][43][44].…”
“…To understand the mechanical behavior of these structures, researchers have been developed various beam theories in recent years, the review of these theories can be found in [1]. There are a number of beam theories which have presented the kinematics of deformation.…”
This paper is dedicated to present static behaviour of Reddy-Bickford laminated composite and sandwich beams subjected to various sets of boundary conditions which are simply supported (SS), clamped-simply supported (CS), clamped-clamped (CC) and clamped-free (CF) by using Ritz method. An analytical solution based on polynomial series including auixiliary functions which are used to satisfy the boundary conditions is developed to solve the studied problem. The polynomial shape functions for axial, transverse deflections and the rotation of the crosssection are presented. The validation and convergence studies are performed by solving symmetric and antisymmetric cross-ply composite beam problems with various boundary conditions and aspect ratios. The numerical results in terms of mid-span deflections, axial and shear stresses are obtained to make comparison with previous studies and to investigate the accuracy of the present study. The effects of fiber angle, lay-up and aspect ratio on displacements and stresses are studied. The static response of the various laminated composite sandwich structures which have symmetric lay-up based on the various boundary conditions, fiber angles and thickness ratios is also studied. It is found that the polynomial series with auxiliary functions can be used for the static analysis of the composite and sandwich beams via Ritz method.
“…Due to the attractive properties in strength, stiffness and lightness, various beam theories have been developed to understand the mechanical behavior of these structures during the last decade. In [1], the review of these theories can be found.…”
Section: Introductionmentioning
confidence: 99%
“…In [1], the trigonometric series solutions are presented for the static, buckling and free vibration responses of laminated composite beams. The vibration analysis of cross-ply laminated beams subjected to different sets of boundary conditions based on a three-degree-of-freedom shear deformable beam theory via Ritz method is presented in [37].…”
In the present paper, the bending behaviour of laminated composite and sandwich beams subjected to various sets of boundary conditions which are simply supported (SS), clamped-simply supported (CS), clamped-clamped (CC) and clampedfree (CF) are investigated by using the Timoshenko beam theory and the Ritz method. In order to solve the problem, the shape functions for axial, transverse deflections and the rotation of the cross-section are presented in polynomial forms. The validation and convergence studies are performed by solving symmetric and anti-symmetric cross-ply composite beam problems with various boundary conditions and aspect ratios by adding auxiliary functions to the shape functions. The results in terms of mid-span deflections, axial and shear stresses are compared with those from previous studies to validate the accuracy of the present study. The effects of fiber angle, lay-up and aspect ratio on displacements and stresses are studied.
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