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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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1 - Compute the centre of the bottom and top endplate, and <br />

<br />

+ <br />

2 - Compute the disc centre, = ( )/2<br />

3 - Loop over the elements of the AF<br />

.1 - Compute the position of the integration points for each element<br />

.2 - Loop over the integration points, .1 - Computation of , Figure 1.b<br />

.1 - Read and store the coordinates of the nodes which lay on the same plane (same<br />

z-coordinate) for the internal and external surfaces, ± ∆z (e.g seed size)<br />

.2 - Resampling of the points of the external and internal surfaces of the AF<br />

<br />

.3 - Compute the temporary centre disc cross-section, .4 - Definition of sets of n points around on the external, , and internal<br />

surfaces, <br />

.5 - Definition of polynomial curves of order n (e.g. second order) by fitting over<br />

the , , and the , <br />

<br />

.6 - Compute the line over and and its intersection with and , <br />

<br />

and .7 - Compute the vectors tangent at the intersection points, and <br />

.8 - Compute the distance = | − | and = | − |<br />

.9 - Determine = + − / .2 - Computation of , Figure 1.c<br />

<br />

and ,<br />

.1 - Compute the angle between x-axis and the line over the .2 - Rotation of of the AF elements to have aligned over x-axis<br />

.3 - Selection of the nodes within a certain offset ± ∆y (e.g. seed size)<br />

<br />

.4 - Repeat steps 3.2.1.4 – 9 using the instead of to determine <br />

⁞<br />

<br />

.10 - Determine by rotation of − of .3 - Determine = × .4 - Rotation of ± around of , where is the fibre angle with respect the<br />

transversal plane, (30°). The sign of has to be chosen according to the number<br />

of layers described and the relative position of in the AF. The rotated represents the fibre orientation at , fibre<br />

.5 - Storing of the element number, the integration number and the fibre components.<br />

4 - Write in a file the fibre orientation per integration point or per element (average and<br />

normalization)<br />

Box.1 Algorithm to compute fibre direction<br />

homogeneous, slightly compressible material, = 0.45, Eq.(2). The embedded collagen<br />

fibres were described by a polynomial formulation [2], Eq. (3). The material<br />

components of the fibres have been modelled as reacting only to elongation.<br />

<br />

(1) = ̅ − 3 + <br />

− 1<br />

<br />

(2) () = ̅ − 3 + ̅ − 3 + <br />

<br />

<br />

( − 1)<br />

(3) () = <br />

/ /<br />

− 1 − ln( ) ≥ 1 , 0 ℎ

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