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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 41
ADVANCES IN THE ANALYSIS AND DESIGN OF COMPOSITES Edited by: B.H.V. Topping
Paper II.3
On Modeling of Global Response Behavior of Sandwich Plates with Laminated Faces M. Di Sciuva and U. Icardi
Department of Aerospace Engineering, Polytechnic of Torino, Torino, Italy M. Di Sciuva, U. Icardi, "On Modeling of Global Response Behavior of Sandwich Plates with Laminated Faces", in B.H.V. Topping, (Editor), "Advances in the Analysis and Design of Composites", Civil-Comp Press, Edinburgh, UK, pp 39-49, 1996. doi:10.4203/ccp.41.2.3
Abstract
The present paper investigates the influence of some non-classical effects (shear deformability of faces, warping of
the cross-section, static continuity requirements at the interfaces)
on deflection, natural frequencies and buckling
loads of sandwich plates with laminated faces. Parametric
studies are performed for different values of the face
thickness/core thickness ratio and of the face transverse
shear flexibility/core transverse shear flexibility ratio by
using smeared laminate models and discrete-layer models.
Also investigated is the effect of the unsymmetry of
faces or of the sandwich plate as a whole. The numerical
results show that the fulfilment of the static continuity
conditions is very important, specially for the standard
sandwich type construction having face layers which behave
as membranes and core layer which only contributes
to the plate transverse shear stiffness.
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