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Composite Materials Research Progress

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In: <strong>Composite</strong> <strong>Materials</strong> <strong>Research</strong> <strong>Progress</strong> ISBN: 1-60021-994-2<br />

Editor: Lucas P. Durand, pp. 165-207 © 2008 Nova Science Publishers, Inc.<br />

Chapter 5<br />

DAMAGE EVALUATION AND RESIDUAL STRENGTH<br />

PREDICTION OF CFRP LAMINATES BY MEANS<br />

OF ACOUSTIC EMISSION TECHNIQUES<br />

Giangiacomo Minak 1 and Andrea Zucchelli 2<br />

Department of Mechanical Engineering, Alma Mater Studiorum - Università di Bologna,<br />

Viale Risorgimento 2, 40135 Bologna, Italia<br />

Abstract<br />

A new approach that integrates acoustic emission (AE) and the mechanical behaviour of<br />

composite materials is presented. Usually AE information is used to evaluate qualitatively the<br />

damage progression in order to assess the structural integrity of a wide variety of mechanical<br />

elements such as pressure vessels. From the other side, the mechanical information, e.g. the<br />

stress-strain curve, is used to obtain a quantitative description of the material behaviour. In<br />

order to perform a deeper analysis, a function that combines AE and mechanical information<br />

is introduced. In particular, this function depends on the strain energy and on the AE events<br />

energy, and it was used to study the behaviour of CFRP composite laminates in different<br />

applications: (i) to describe the damage progression in tensile and transversal load testing; (ii)<br />

to predict residual tensile strength of transversally loaded laminates (condition that simulates a<br />

low velocity impact).<br />

Introduction<br />

Long fibre reinforced composite laminates are a complex structure at the meso-scale. The<br />

fibres embedded in the matrix constitute the lamina and the overlapping of different laminas<br />

makes the composite laminate. A consequence of this architecture is the complex behaviour<br />

during loading and servicing of components realized by such material, and the multiplicity of<br />

different failure mechanisms that determine the damage progression.<br />

1 E-mail address: giangiacomo.minak@unibo.it<br />

2 E-mail address: a.zucchelli@unibo.it

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