• Aucun résultat trouvé

Damage evaluation in composite laminate by theuse of ultrasonic lamb wave

N/A
N/A
Protected

Academic year: 2021

Partager "Damage evaluation in composite laminate by theuse of ultrasonic lamb wave"

Copied!
1
0
0

Texte intégral

(1)

la 3 Conférence Internationale sur le Soudage, le CND et l’Industrie des Matériaux et Alliages (IC-WNDT-MI’12)

2012

Damage evaluation in composite laminate by the use of ultrasonic lamb wave

HALIMI Rafik, BEZZAZI Boudjema, BADIDI BOUDA Ali, ARIBI Choaib

Abstract : This paper presents some ultrasonic methods to detect and to characterize defects, possibly obtained after damage caused in composite materials. Firstly, artificial defects are located by two piezoelectric transducers. A two-dimensional ultrasonic cartography C-scan, performed section by section, at different positions which took part through the thickness of a carbon fiber-reinforced plastic composite beam, to be analyzed. Next, fundamental symmetric S0 mode of Lamb waves is used to measure the size of the delamination by scanning over the surface beneath which a delamination lies. A remarkable decrease in the arrival time due to the delamination is detected, and the delamination length can be calculated based on a simple model for Lamb-wave propagation. Furthermore, the delamination edge is located as a sudden decrease in the amplitude. The rate of decrease in amplitude of an individual pulse cycle was detected to vary with the depth of the delamination, being most sensitive to delaminations near the surface of the plate. This is particularly useful when sizing for defects close to the surface, where a normal-incidence pulse-echo ultrasonic method has problems, particularly when the depth of the defect or the back-wall echoes lie within the length of the transmitted ultrasonic pulse. The technique has potential for faster c-scanning of a complete plate than the usual normal-incidence pulse-echo method.

Keywords : composite, Ultrasonic C-scan, laminate plate, delamination, Lamb waves

Centre de Recherche en Technologies Industrielles - CRTI - www.crti.dz

Powered by TCPDF (www.tcpdf.org)

Références

Documents relatifs

The goal of this work was to determine the longitudinal residual stress distribution in a TIG weld on Ti- 6Al-4V and to compare the stress distribution to the

Abstract : it is necessary to measure this layer with a sufficient precision.In this study, we use the ultrasonic pulse echo method as a non destructive testing in thecementation

between bother the acoustic attenuation and reflection coefficients of longitudinal Ultrasonic waves propagated in samples having different case layer

Using the maximum and minimum values of the received amplitude and arrival times of the transmitted S 0 mode along the Y direction, we were able to identify the

In this context, we develop signal processing tools based on Split Spectrum Processing (SSP) with Q constant method allowing to detect and locate the imperfections present in

This algorithm iterates back and forth using the current estimated parameter in order to decompose the observed data and thus to increase the likelihood of the next

Figure 2 presents a photograph of the debonded areas before the wearing course construction (2a) and a map of the experimental section, with the location of the

The experimental procedure consists to measure ultrasonic pulse velocities through the freshly mixed concrete in the upper and lower parts of samples (fig. 2-c) using