A multiobjective multidisciplinary design optimization (MDO) of two-dimensional airfoil is presented. In this paper, an approximation for the Pareto set of optimal solutions is obtained by using a genetic algorithm (GA). The first objective function is the drag coefficient. As a constraint it is req
Genetic algorithms and fictitious domain based approaches in shape optimization
✍ Scribed by J. Haslinger; D. Jedelský
- Publisher
- Springer-Verlag
- Year
- 1996
- Tongue
- English
- Weight
- 717 KB
- Volume
- 12
- Category
- Article
- ISSN
- 1615-1488
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