Suliman, M. (2011). APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE. test, 11(ASAT Conference, 17-19 May 2005), 31-42. doi: 10.21608/asat.2011.27138
Mutawkil A. Suliman. "APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE". test, 11, ASAT Conference, 17-19 May 2005, 2011, 31-42. doi: 10.21608/asat.2011.27138
Suliman, M. (2011). 'APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE', test, 11(ASAT Conference, 17-19 May 2005), pp. 31-42. doi: 10.21608/asat.2011.27138
Suliman, M. APPLICATION OF GENETIC ALGORITHMS WITH THE AID OF PANEL METHOD TO OPTIMIZE MISSILE AERODYNAMIC SHAPE. test, 2011; 11(ASAT Conference, 17-19 May 2005): 31-42. doi: 10.21608/asat.2011.27138

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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