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ARUP; ISBN: 978-0-9562121-5-3 - CMBBE 2012 - Cardiff University

ARUP; ISBN: 978-0-9562121-5-3 - CMBBE 2012 - Cardiff University

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z<br />

y<br />

x<br />

z<br />

z<br />

x<br />

(c)<br />

y<br />

x<br />

(d)<br />

Figure 1. 3D sketch of the IVD (a); sketch for computation of (b); sketch for<br />

<br />

computation of (c); FE model (d) with tetrahedral, λ=2, (left) and hexahedral<br />

mesh, λ=8, (right).<br />

<br />

<br />

[MPa] [MPa] [MPa] [MPa] [MPa]<br />

<br />

-<br />

<br />

[MPa]<br />

0.0033 67.02 0.036 0.069 2.16 0.093 53.23<br />

Table 1. Finite element<br />

model properties.<br />

Where is the right Cauchy-Green deformation tensor, is the deformation<br />

gradient tensor measure of the transformation, det is the Jacobian determinant, a<br />

measure of the volume change. ̅ is the first invariant of the deviatoric deformation<br />

tensor / and is the square of the fibre stretch.<br />

, , , , , and , are the material coefficients for the NP and the AF,<br />

see Table 1. The constitutive equations have been implemented in the ABAQUS finite<br />

element package (ABAQUS 6.9.3, Hibbit, Karlsson and Sorenson Inc., Pawtucket, RI,<br />

USA) with FORTRAN subroutines and tested through simple FE models. Linear fullyintegrated<br />

hexahedral elements (C3D8) and second order fully-integrated elements<br />

(C3D10) were used for the discretization of the system. The seed size was chosen by<br />

dividing the disc height by a factor λ. For the hexahedral mesh, we have chosen λ = 8,<br />

whereas λ = 2, 4, 6, 8 were used for the tetrahedral element models. We assumed the AF<br />

to be comprised of eight alternating layers, with the fibre orientation described as in<br />

Holzapfel et al. [15]. The study cases were: Axial compression (-1mm), flexion (5°),<br />

torsion (5°) and lateral bending (5°). A pre-stress analysis was implemented prior to the<br />

studies to compute the stress distribution induced by a swelling pressure of 0.1MPa.<br />

4. RESULTS<br />

(a)<br />

The load-displacement curves obtained from the tetrahedral and hexahedral mesh<br />

models showed a comparable disc response (Figure 2.a). The model with a coarse<br />

tetrahedral mesh (λ=2) showed similar results to the hexahedral mesh in axial<br />

compression (max. error 4.6%) and flexion (max. error 6.1%) when responses were<br />

compared at the organ level. However, the coarse tetrahedral model started to diverge<br />

when lateral bending greater than 2.5° was applied (max. error 17.6%). This was<br />

improved by using a model with a finer tetrahedral mesh (λ=4). For torsion, both<br />

y<br />

x<br />

(b)

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