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
Missile Aerodynamic Shape Optimization Using Genetic Algorithms
โ Scribed by Anderson, M. B.; Burkhalter, J. E.; Jenkins, R. M.
- Book ID
- 126268352
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2000
- Tongue
- English
- Weight
- 314 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0022-4650
- DOI
- 10.2514/2.3615
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