11.02.2013 Views

Computational Methods for Debonding in Composites

Computational Methods for Debonding in Composites

Computational Methods for Debonding in Composites

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

6 Study of Delam<strong>in</strong>ation with <strong>in</strong> <strong>Composites</strong> 127<br />

material is completely damaged, d = 1. The effective stresses, shown <strong>in</strong> Eq. (6.22),<br />

correspond to the stresses that would be obta<strong>in</strong>ed <strong>in</strong> the material if it is not<br />

damaged:<br />

σσσ 0 = C0 : εεε (6.23)<br />

And the real stress tensor can be obta<strong>in</strong>ed, from the stra<strong>in</strong> state of the material,<br />

by coupl<strong>in</strong>g Eqs. (6.22) and (6.23).<br />

6.2.3.2 Damage Criterion<br />

σσσ =(1 − d)σσσ0 =(1 − d)C0 : εεε (6.24)<br />

The damage criterion predicts when the damage process beg<strong>in</strong>s to take place <strong>in</strong><br />

the material, this is: when the material elastic behaviour is lost as a result of the<br />

degradation. This criterion is used to represent different material behaviours, and it<br />

depends on the stress tensor and on the value of the <strong>in</strong>ternal variables found <strong>in</strong> the<br />

material po<strong>in</strong>t under study. Its expression is:<br />

F(σσσ 0, q)= f (σσσ 0) − c(d) ≤ 0 with q ≡{d} (6.25)<br />

where c(d) is a function def<strong>in</strong><strong>in</strong>g the damage limit value and f (σσσ 0) def<strong>in</strong>es the damage<br />

surface. Damage will start the first time that f (σσσ 0) value is equal or larger than<br />

c(d). Usually, <strong>in</strong>stead of work<strong>in</strong>g with Eq. (6.25), the damage criterion is converted<br />

to an equivalent one by us<strong>in</strong>g a scalar function G which is positive and with its<br />

derivative positive, monotonously <strong>in</strong>creas<strong>in</strong>g and <strong>in</strong>vertible:<br />

F ∗ (σσσ 0,d)=G[ f (σσσ 0)] − G[c(d)] ≤ 0 (6.26)<br />

The damage surface to be used with this <strong>for</strong>mulation can be any of the exist<strong>in</strong>g <strong>in</strong><br />

literature (i.e. Von-Mises, Mohr-Coulomb, etc.) and its election will depend on the<br />

material to be modeled. In the present work, the damage surface that will be used<br />

<strong>for</strong> matrix material corresponds to the one def<strong>in</strong>ed by norm of pr<strong>in</strong>cipal stresses,<br />

weighted accord<strong>in</strong>g to the compression–tension proportion found <strong>in</strong> the pr<strong>in</strong>cipal<br />

stress tensor. This damage surface can be written as:<br />

f (σσσ 0)=ρ ·�σσσ I� (6.27)<br />

be<strong>in</strong>g σσσ I the pr<strong>in</strong>cipal stress tensor and ρ the compression–tension weight function,<br />

def<strong>in</strong>ed as:<br />

ρ = r0N +(1 − r0) (6.28)<br />

where N = σ max<br />

t is the material ratio between the maximum accepted compressive<br />

strength/tensile strength. And r0 is a scalar function that def<strong>in</strong>es the relation<br />

c /σ max

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!