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, Page 31-42 PDF (1.83 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2011.27138 | ||||
 View on SCiNiTO | ||||
| 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 | ||||
|
Statistics Article View: 148 PDF Download: 240 |
||||
