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Computational Methods for Debonding in Composites

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4 Analytical and Numerical Investigation of the Length of Cohesive Zone 79<br />

τ = τ o<br />

� �n x<br />

(4.2)<br />

lcz<br />

where n is a material parameter.<br />

In the elastic zone, the traction profile follows the expression given by the L<strong>in</strong>ear<br />

Elastic Fracture Mechanics (LEFM) solution:<br />

τ =<br />

KI<br />

� 2π (x − r1)<br />

(4.3)<br />

The size of the <strong>in</strong>elastic zone, lcz, also called cohesive zone or fracture process<br />

zone, is obta<strong>in</strong>ed by assum<strong>in</strong>g that the traction given by Eqs. (4.2) and (4.3) must be<br />

equal at x = lcz, and that the areas A1 and A2 represented <strong>in</strong> Fig. 4.1 are equal [2].<br />

Assum<strong>in</strong>g that there are no size effects, the crack propagates when the stress <strong>in</strong>tensity<br />

factor KI equals to the critical value KIc. There<strong>for</strong>e, the size of the cohesive zone<br />

when the crack is propagat<strong>in</strong>g <strong>in</strong> a self-similar way can be solved us<strong>in</strong>g the previous<br />

equations, result<strong>in</strong>g <strong>in</strong>:<br />

l ∞ cz =<br />

n + 1<br />

π<br />

K 2 Ic<br />

(τ o ) 2<br />

(4.4)<br />

Cox and Marshall [5] proposed an alternative approach to predict the length of<br />

the cohesive zone. The Cox and Marshall [5] model is based on the concept of a<br />

bridged crack, where the length of the bridg<strong>in</strong>g zone is calculated by impos<strong>in</strong>g two<br />

Fig. 4.1 Stress profile ahead of the crack tip

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