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dissertation global and local fracture properties of metal matrix ...

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Section 3<br />

Fig. 3.6. Schematic view <strong>of</strong> the HRR-theory.<br />

21<br />

(3.1)<br />

In Eq. 3.1, E is the Young modulus, J is the <strong>fracture</strong> toughness <strong>of</strong> material, σ0 is the yield<br />

strength, r <strong>and</strong> θ are the polar coordinates, IN <strong>and</strong> dN are dimensionless constants both<br />

depending on the strain hardening coefficient, N, <strong>and</strong> on σ0 /E, ~ σ ( N,<br />

θ ) is a dimensionless<br />

function listed in [59].<br />

The J-integral in Eq. 3.1 can be substituted by COD using the relation proposed by Shih in<br />

[58]<br />

, (3.2)<br />

where dN is dimensionless constant depending on the strain hardening coefficient, N, [58].<br />

The material is assumed to follow a st<strong>and</strong>ard power-law work hardening behavior<br />

, (3.3)<br />

where according to [59], the σ0 is set to the yield strength, σy, <strong>and</strong> α is determined from the<br />

tensile true stress-strain curve.<br />

⎡ E J ⎤<br />

σ σ<br />

~<br />

ij = 0 ⎢<br />

σ ,<br />

2 ⎥<br />

ij<br />

⎢⎣<br />

ασ 0 I N r ⎥⎦<br />

J =<br />

d<br />

1<br />

σ 0<br />

N<br />

To evaluate the stress tensor at the moment <strong>of</strong> void initiation, σ HRR vi, the measured r, θ, <strong>and</strong><br />

the CODvi-values are inserted into Eqs. (3.2) <strong>and</strong> (3.1). From the stress tensor σ HRR vi, the<br />

maximum principal stress, σ HRR max, can be calculated.<br />

1/(<br />

N + 1)<br />

COD<br />

ε<br />

⎛ σ ⎞<br />

= α ⎜<br />

⎟<br />

ε 0 ⎝σ<br />

0 ⎠<br />

N<br />

r<br />

θ<br />

( N θ )<br />

ij<br />

σij

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