Numerical assessment of the core deformability effect on the behavior of sandwich beams

A modified zig-zag technical theory suitable for the accurate analysis of m ulti-layered composite beams accounting for the full 3D stress state has be en recently developed by one of the authors [U. Icardi, A three-dimensional zig zag theory for analysis of thick laminated beams. In: Modern Trends in the Theory and Behavior of Structures Symposium ASME 1999 Summer Conferenc e, Blacksburg, Virginia, USA, 27- 30 June 1999]. In order to satisfy the tr ansverse shear and the transverse normal stress and stress gradient continu ity requirements at the laminae interfaces through appropriate jumps in the strains, the theory features a piecewise third-order approximation for the in-plane displacement and a fourth-order approximation for the transverse displacement across the thickness. In the present paper, the capability of such a theory to predict the displacement and stress distribution across th e thickness of sandwich beams is numerically assessed. This is done by comp aring present estimates with the Pagano's elasticity solution [N.J. Pagano, J. Compos. Mater. 3 (1969) 398-411] for simply-supported, sandwich beams w ith cross-ply faces, loaded by a sinusoidally distributed transverse load. Additional results are presented that evidence the effects played by an enh anced core's deformability, or by stiffening the faces. It is seen from the numerical results presented the need for including non-classical complicat ing effects, to accurately predict the stress and displacement distribution s across the thickness, and even for the estimation of the overall response . These comprise modeling of the transverse normal strain and transverse sh ear deformation; fulfillment of the transverse shear stress and transverse normal stress and stress gradient continuity conditions at interfaces; mode ling of the cross-section warping. The numerical results show a good predic tive capability of the present model with using one sublaminate for each la yer and for the core, except for the case of faces with drastically differe nt elastic moduli, which require use of more sublaminates. (C) 2001 Elsevie r Science Ltd. All rights reserved.