On the Rigidity in Bending of a Sandwich with Thick CFRP Facings and Thin Soft Core G. Caprino & P. Iaccarino & A. Langella & A. Lamboglia Received: 16 January 2009 / Accepted: 30 March 2009 / Published online: 16 April 2009 # Springer Science + Business Media B.V. 2009 Abstract Flexure tests in three-point bending were performed in the elastic domain on sandwich specimens whose facings were made of T800H/3900-2 laminates, and the core by a soft rubbery layer. The contribution of the shear and flexural deformations to the overall deflection was varied by varying the slenderness ratio. The rigidities yielded by the load- displacement curve were corrected for the indentation occurring at the points of load introduction, using an experimentally determined calibration curve. Due to the thinness of the sandwich, indentation negligibly affected the precision of the results, with the apparent rigidities differing from the actual ones by less than 2%. By an analytical formula previously developed for sandwich structures, a prediction of the rigidities in flexure was attempted, adopting elastic constants available in the literature. The correlation with the data points was poor, with the theoretical results largely overestimating the actual rigidities. However, the reliability of the closed-form formula was supported by finite element analysis, carried out modelling the facings by 2D plate elements, and the core by 3D brick elements. Through the formula, the core shear modulus was individuated as responsible of the discrepancies observed. Assuming a suitable value for this parameter, both the analytic solution and the finite element models were able to match with accuracy the rigidities measured. Keywords Polymer-matrix composites . Mechanical properties . Finite element analysis . Elastic properties . Sandwich with soft core 1 Introduction Making more comfortable, low cost, environmentally friendly aircraft is the goal of the aeronautical designers for the next generation commercial fleets. Carbon-Fibre-Reinforced Plastics (CFRPs) play a key role in the achievement of these tasks, allowing considerable weight Appl Compos Mater (2009) 16:163–172 DOI 10.1007/s10443-009-9084-8 G. Caprino : P. Iaccarino (*) : A. Langella Department of Materials and Production Engineering, University of Naples “Federico II”, Piazzale Tecchio, 80, 80125 Naples, Italy e-mail: paiaccar@unina.it A. Lamboglia Alenia Aeronautica, Viale dell’Aeronautica, 80038 Pomigliano d’Arco, Italy