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The use of genetic algorithms with the aid of the panel method to determine high-efficiency missile aerodynamic shape has been examined. The capability of these algorithms to determine highly efficient and robust missile aerodynamic designs is demonstrated by giving a variety of design variables and constraints. Results indicate that the genetic algorithm is clearly capable of designing aerodynamic shapes that perform well in either single or multiple goal applications.

APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE