Abstract
This paper examines the adequacy of first order shear deformation theory (FSDT) based layered shell finite element by comparing with 2D and 3D models without imposing any constraint on the deformation behaviour of core. The effect of core compressibility and transverse flexibility in the behaviour of sandwich beams are studied. Plane and 3D models are able to capture the higher order shear stress variation across the thickness of core, whereas classical models and layered models results in constant shear stress across the thickness of the core. Results of the finite element models indicate the necessity of shear correction factor for rigid core considering shear strain energy criteria or average shear strain criteria, whereas for soft core, the shear correction factor is unity (=1).
Highlights
Sandwich structures composed of two thin, strong and stiff facing sheets separated by a thick, lightweight core (Figure 1), are extensively used in aerospace industry due to their low density and high specific stiffness and strength
Majority of sandwich finite elements use refinements of the classical lamination theory (CLT) with first order shear deformation theory (FSDT), whereas the higher order shear deformation models are based on equivalent single layer (ESL) approach
Finite element analysis has been carried out on three-point sandwich beam to examine the influence of core compressibility, flexibility and transverses shear by varying core modulus and thickness
Summary
Influence of Core Compressibility, Flexibility and Transverse Shear Effects on the Response of Sandwich Structures. Received: October 15, 2016; Accepted: December 6, 2016; Published: January 21, 2017
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have