Paper Titles

Fracture Toughness Characterization of Carbon Bonded Alumina Using Chevron Notched Specimens
p.71

Experimental Study of Fatigue Crack Initiation and Strain Evolution around a Micro-Void by In Situ SEM and Digital Image Correlation
p.75

Experimental Characterization of Competition of Surface and Internal Damage in Very High Cycle Fatigue Regime
p.79

Influence of the Crack Widening on the Transverse Cracking in Lamellar Metal-Ceramic Composites
p.83

Buckling and Post-Buckling Behaviour of Impacted Glass Reinforced Composite Plates under Compression after Impact Tests
p.87

The Evaluation of Deformation and Fracture of Gilsocarbon Graphite Subject to Service Environments: Experimental and Modelling
p.91

Effect of Shrinkage Porosity and Degenerated Graphite on Fatigue Crack Initiation in Ductile Cast Iron
p.95

Fracture-Mechanics Behaviour of Ceramic Foam with Macroscopic Stress Concentrator upon the Tensile Test
p.99

3D Model of Crack Propagation in Particulate Ceramic Composite Containing Residual Stresses
p.103

HomeKey Engineering MaterialsKey Engineering Materials Vol. 754Buckling and Post-Buckling Behaviour of Impacted...

Buckling and Post-Buckling Behaviour of Impacted Glass Reinforced Composite Plates under Compression after Impact Tests

Article Preview

Abstract:

The present work deals with the Compression After Impact numerical simulations on low velocity impacted glass fibre reinforced composite plates configurations characterised by three different stacking sequences. The damaged numerical FEM models, deriving from impact explicit analyses, have been used as an input to perform explicit analyses simulating the compressive test. The drop, in terms of compressive residual strength, is analysed and discussed. Considerations on the buckling and post-buckling behaviour of these plates under compression are then introduced.

You might also be interested in these eBooks

Advances in Fracture and Damage Mechanics XVI

Info:

Periodical:

Key Engineering Materials (Volume 754)

Pages:

87-90

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.754.87

Citation:

Cite this paper

Online since:

September 2017

Authors:

Roberta Cristiano*, Gaetano Perillo

Keywords:

CAI, Composite, GFRP

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

© 2017 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] A. Riccio, C. Di Costanzo, P. Di Gennaro, A. Sellitto, A. Raimondo. Intra-laminar progressive failure analysis of composite laminates with a large notch damage. Engineering Failure Analysis 2017; 73: 97-112.

DOI: 10.1016/j.engfailanal.2016.12.012

[2] S. Abrate. Impact on composite structures. Cambridge University Press 1998: 289.

[3] A. Raimondo, A. Riccio. Inter-laminar and intra-laminar damage evolution in composite panels with skin-stringer debonding under compression. Composites Part B: Engineering 2016; 94: 139-151.

DOI: 10.1016/j.compositesb.2016.03.058

[4] A. Riccio, M. Damiano, A. Raimondo, G. Di Felice, A. Sellitto. A fast numerical procedure for the simulation of inter-laminar damage growth in stiffened composite panels. Composite Structures 2016; 145: 203-216.

DOI: 10.1016/j.compstruct.2016.02.081

[5] R. Borrelli, A. Riccio, A. Sellitto, F. Caputo, T. Ludwig. On the use of global-local kinematic coupling approaches for delamination growth simulation in stiffened composite panels. Composites Science and Technology 2015; 115: 43-51.

DOI: 10.1016/j.compscitech.2015.04.010

[6] A. Riccio, S. Saputo, A. Sellitto. A user defined material model for the simulation of impact induced damage in composite. Key Engineering Materials 2016; 713: 14-17.

DOI: 10.4028/www.scientific.net/kem.713.14

[7] F. Caputo, G. Lamanna, A. De Luca, R. Borrelli, S. Franchitti. Global-Local FE Simulation of a Plate LVI Test; Structural Durability & Health Monitoring. TechScience 2013; 9(3): 253-267.

DOI: 10.32604/sdhm.2013.009.253

[8] F. Caputo, A. De Luca, G. Lamanna, V. Lopresto, A. Riccio. Numerical investigation of onset and evolution of LVI damages in Carbon-Epoxy plates. Composite Part B: Engineering 2015; 68: 385-391.

DOI: 10.1016/j.compositesb.2014.09.009

[9] R. Sepe, A. De Luca, G. Lamanna, F. Caputo. Numerical and experimental investigation of residual strength of a LVI damaged CFRP omega stiffened panel with a cut-out. Composites Part B: Engineering 2016; 102: 38-56.

DOI: 10.1016/j.compositesb.2016.07.009

[10] A. Turon, P.P. Camanho, J. Costa, C.G. Dávila. A damage model for the simulation of delamination in advanced composites under variable-mode loading. Mechanics of Materials 2006; 38(11): 1072-89.

DOI: 10.1016/j.mechmat.2005.10.003

[11] C. Bouvet, B. Castanié, M. Bizeul, J. -J. Barrau. Low velocity impact modelling in laminate composite panels with discrete interface elements. International Journal of Solids and Structures 2009; 46(14–15): 2809-21.

DOI: 10.1016/j.ijsolstr.2009.03.010

[12] S. Rivallant, C. Bouvet, N. Hongkarnjanakul. Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements. Composites Part A: Applied Science and Manufacturing 2013; 55: 83-93.

DOI: 10.1016/j.compositesa.2013.08.003

[13] A. Riccio, R. Ricchiuto, F. Di Caprio, A. Sellitto, A. Raimondo. Numerical investigation of constitutive material models on bonded joints in scarf repaired composite laminates. Engineering Fracture Mechanics 2017; 173: 91-106.

DOI: 10.1016/j.engfracmech.2017.01.003

[14] G. Perillo, R. Cristiano, A. Riccio. A Numerical/Experimental study on the impact and CAI behaviour of Glass Reinforced Composite plates. Submitted.

DOI: 10.1007/s10443-017-9628-2

[15] Abaqus 6. 14: Analysis User's Manual.