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Composite Materials Research Progress

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76<br />

Michaël Bruyneel<br />

The symbols ∑ ( +) and ∑ ( −) in (7.3) denote the summations over terms having positive<br />

and negative first order derivatives. When the first order derivative of the considered<br />

structural response is positive a linear approximation in terms of the direct variables is built,<br />

while a reciprocal approximation is used on the contrary.<br />

145<br />

140<br />

135<br />

130<br />

125<br />

120<br />

115<br />

110<br />

105<br />

100<br />

g(x<br />

)<br />

~ ( )<br />

g k<br />

l<br />

( x)<br />

Strain energy density<br />

(N/mm)<br />

~ ( )<br />

g k<br />

r<br />

( x)<br />

45 90 (k )<br />

(k )<br />

180<br />

xr<br />

xl<br />

Figure 7.2. The Conlin approximation.<br />

Conlin can only work with positive design variables since an asymptote is imposed at<br />

xi=0. On top of that, the curvature of this approximation is imposed by the derivative at the<br />

current design point and can not be adapted to better fit the problem.<br />

The Method of Moving Asymptotes or MMA (Svanberg 1987) generalizes Conlin by<br />

introducing two sets of new parameters, the lower and upper asymptotes, Li and Ui, that can<br />

take positive or negative values, in order to adjust the convexity of the approximation in<br />

accordance with the problem under consideration. The asymptotes are updated following<br />

some rules provided by Svanberg (1987). The parameters pij and qij are built with the first<br />

order derivatives.<br />

Strain energy<br />

145 density (N/mm)<br />

140<br />

135<br />

130<br />

125<br />

120<br />

115<br />

110<br />

105<br />

g(x<br />

)<br />

~ ( )<br />

g ( x)<br />

k<br />

100<br />

(k )<br />

L<br />

100<br />

(k )<br />

U<br />

45 90 (k ) 135 (k )* 180 45 90 (k )*<br />

(k )<br />

180<br />

x<br />

x<br />

Strain energy<br />

145 density (N/mm)<br />

140<br />

135<br />

130<br />

125<br />

120<br />

115<br />

110<br />

105<br />

g(x<br />

)<br />

Figure 7.3. The MMA approximation.<br />

x<br />

~ ( )<br />

g ( x)<br />

k<br />

x

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