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Damage tolerance of impacted curve composite structures : scale effects

Ballere, Ludovic (2008) Damage tolerance of impacted curve composite structures : scale effects. PhD thesis Mécanique, LAMEFIP, ENSAM 2008ENAM0010 p.209.

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Abstract

During its life, a composite structure can be damaged locally although this deterioration may not be visible to the naked eye. It is necessary, in the stage of design, to appreciate the criticality of such a damage. Nevertheless, tests needed to estimate this criticality are often very expensive, especially in the case of large-size parts. The use of small-scale models can be an alternative to this problem. That implies the use, even the development, of scaling methods making it possible to extrapolate the behaviour of the reduced structure to that of the real structure. The objective of this research work, realized in collaboration between the laboratory LAMEFIP-ENSAM-ParisTech and SNECMA Propulsion Solide SAFRAN Group, is to establish a methodology that would potentially free the compagny from a heavy experimental study on structures (filament wound vessels) at the real scale. From tests, carried out on structures at smaller scales and from the model established in this work, it will be possible to predict the residual behaviour under internal pressure of a structure at the real scale when it is damaged by impact. Curved panels were used for the establishment of this methodology since they are less expensive than filament wound vessels - even at reduced scale -. Initially, a damage tolerance study, consisting of damage initiation by impacts, ultrasonic and microscopic inspections of the damage and quasi-static tensile tests until rupture, was carried out on two sclaes of specimens, based on experimental designs. Through this study, it was possible to highlight the existence of many scale effects, mainly due to the thickness and the curvature of the specimens. Then, a progressive damage model of the layers and the interface was established and implemented in a finite element code and fine tuned with respect to the response surfaces experimentally determined. This numerical modeling establishes the methodology allowing the scaling of structures. Then, this methodology was applied to the case of filament wound vessels. Numerical results match with data of an experimental study carried out on scaled vessels and show the need for taking into account the damage of the interface for the prediction of the residual behaviour of pre-impacted curved structures.

Item Type:PhD Thesis (PhD)
PhD Supervisor:Lataillade, Jean-Luc
Date:20 May 2008
Board of examiners:Pierron, Fabrice and Lafarie-Frenot, Marie-Christine and Carrere, Nicolas and Barrau, Jean-Jacques and Lataillade, Jean-Luc and Viot, Philippe and Cloutet, Sébastien
Ecole Doctorale:ED 432 ECOLE DOCTORALE SCIENCES DES METIERS DE L'INGENIEUR
Discipline:Mécanique
Collection (Fonds):Arts et Métiers ParisTech (ENSAM)
Institution:ENSAM
Department:LAMEFIP
Subjects:4. Materials Science, Mechanics and Mechanical Engineering
Uncontrolled Keywords:Eprouvettes courbes, Matériaux composites, Impact, Comportement résiduel en traction, Effets d'échelles, Capacités bobinées, Modèle d'endommagement progressif, Eléments cohésifs, Curved panels, Composite materials, Impact, Residial tensile behaviour, Scale effects, Filament wound vessels, Progressive damage modelling, Cohesive elements
ID Code:4191
Deposited By:Ludovic Ballere
Deposited On:06 October 2008

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