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ALJOIN Final Technical Report - Transport Research & Innovation ...

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Contract N° G3RD-CT-2002-00829<br />

<strong>Final</strong> <strong>Technical</strong> <strong>Report</strong> – draft 1<br />

<strong>ALJOIN</strong> The numerical analyses were carried out using the both the LS-DYNA explicit code and<br />

the FRANC2D code. Figure 16 shows the results of the analysis, in terms of distribution<br />

of the Von Mises equivalent stress, demonstrating the crack propagation along the<br />

centreline of the specimen. Figure 17 shows the results of the simulations done using<br />

the FRANC2D code 1 which allows to explicitly model the crack propagation in the mesh.<br />

As the cracks propagate, automatic remeshing algorithms delete the mesh local to the<br />

crack tip, extend the crack, and build a new mesh around the new tip. The constant<br />

critical crack tip opening angle (CTOA) fracture criterion was used in the simulations.<br />

The CTOD fracture criterion assumes that the crack growth will occur when the angle<br />

made by the upper crack surface, the crack tip, and the lower crack surface reaches a<br />

critical value. In a two-dimensional analysis, the displacement δ, perpendicular to the<br />

crack, at a fixed distance d behind the crack tip are monitored during the analytical<br />

loading of the model. When the displacements are such that the critical angle CTOA<br />

(ψC) is attained (see equation 1), the crack is advanced by releasing the crack tip nodes<br />

until a total distance d of crack growth is achieved.<br />

−1⎛<br />

δ ⎞<br />

ψ C = 2 tan ⎜ ⎟<br />

(1)<br />

⎝ d ⎠<br />

Then, the applied displacements are held constant while the internal forces are returned<br />

to equilibrium. At each load increment, the CTOA was calculated and compared to a<br />

critical value. When the CTOA exceeded this critical value, the crack-tip node was<br />

released and the crack advanced.<br />

t = 0.6 s<br />

t = 2.0 s<br />

Figure 16 Numerical Analysis of Crack Tip Opening (CTOA) tearing tests (Von Mises<br />

Equivalent Stress)<br />

1 Swenson D., James M., “FRANC2D/L: A Crack Propagation Simulator for Plane Layered Structures<br />

Version 1.4 User's Guide”, Kansas State University •Manhattan, Kansas<br />

20

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