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Quantitative a posteriori error estimators in Finite Element-based shape optimization

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Academic year: 2021

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Figure

Figure 1 – Conception d’un m´ecanisme inverseur compliant ` a l’it´eration 100 et 1562
Figure 2 – Section transversale d’un fuselage d’Airbus A300. On remarque les trous circulaires dans la poutre.
Figure 5 – Conception d’une aile pour diff´erentes phases de vol. (a) D´ecollage - Surface de l’aile augment´ee
Figure 6 – Snapshots of compliant inverter design at iteration 100 and 1562. The objective function of the final design (b) is 5.5% better than at 100 iterations (a)
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