APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE | ||
| International Conference on Aerospace Sciences and Aviation Technology | ||
| Article 3, Volume 11, ASAT Conference, 17-19 May 2005, May 2011, Pages 31-42 PDF (1.83 M) | ||
| Document Type: Original Article | ||
| DOI: 10.21608/asat.2011.27138 | ||
| Author | ||
| Mutawkil A. Suliman | ||
| Eng., Lecturer, Dpt. Of Mech. Aeronautical & Aerospace, Karary Academe of Technology, Khartoum, Sudan. | ||
| Abstract | ||
| 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. | ||
| Keywords | ||
| Genetic Algorithm; Panel method; Missile; Optimization; CFD; Aerodynamic shape | ||
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