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Composite Materials Research Progress

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96<br />

Michaël Bruyneel<br />

a solution with SAM is reached in 6 iterations, while Conlin is still no longer able to<br />

converge.<br />

8.6. Topology Optimization of Laminated <strong>Composite</strong> Structures<br />

The topology optimization problem of Figure 4.3 is here considered. In topology optimization<br />

of isotropic material (Bendsoe 1995), the design variable is a pseudo-density μi that varies<br />

between 0 and 1 in each finite element i (Figure 4.2). The so-called SIMP material law<br />

(Simply isotropic Material with Penalization) takes the following form:<br />

Ei<br />

= μ<br />

p 0<br />

i E<br />

0<br />

ρi = μi<br />

ρ<br />

(8.5)<br />

where E 0 and ρ 0 are the Young modulus and the density of the base material (e.g. steel), E<br />

and ρ are the effective material properties, and p is the exponent of the SIMP law, chosen by<br />

the user (1

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