Titresimli Genetik Algoritma ile Hizlandirilmis ... - Hava Harp Okulu

Titresimli Genetik Algoritma ile Hizlandirilmis Kanat Profili Optimizasyonuy/cx/cSekil 12: Optimize edilen profil için M=0.75 ve 2? hücum açisinda (Reynolds sayisiRe c =6.5x10 6 ) es-basinç katsayisi çizgileri (Durum-b).Uygunluk (L/D)6560555045ST-I40ST-II3530250 500 1000 1500 2000HAD Hesabi SayisiSekil 13: TGA (ST-II) ve klasik GA (ST-I) ile yapilan optimizasyonsüreçlerinin karsilastirilmasi (Durum-b).9. Kaynaklar[1] Falco, I. D., Cioppa, A. D., Balio R. D. andTarantino, E., “Breeder Genetic Algorithms for AirfoilDesign Optimisation”, IEEE Int. Conf. OnEvolutionary Computing, Nagoya, Japan, 1996.[2] Mühlenbein, H. and Schlierkamp -Voosen, D.,“Predictive Models for the Breeder Genetic AlgorithmI. Continuous Parameter Optimization”, EvolutionaryComputation 1, pp. 25-49, 1993.[3] Falco, I. D., Cioppa, A. D., Lazzetta A. andTarantino, E., “M ijn Mutation Operator for AirfoilDesign Optimisation”, Soft Computing in EngineeringDesign and Manufacturing, Springer Verlag, pp. 211-220, 1998.[4] Vicini, A. and Quagliarella, D., “Airfoil and WingDesign Through Hybrid Optimization Strategies”, AIAAJournal, Vol. 37, No. 5, 1999.[5] Tse, D.C.M., and Chan, L.Y.Y., “Application of MicroGenetic Algorithms and Neural Networks for AirfoilDesign Optimization”, RTO MP-035 RTO-MP-035Aerodynamic Design and Optimisation of Flight Vehiclesin a Concurrent Multi-Disciplinary Environment, 1999.[6] Hacioglu, A. and Özkol, I., “Vibrational GeneticAlgorithm as a New Concept in Aerodynamic Design”,Aircraft Engineering and Aerospace Technology, Vol. 74,No. 3, pp. 228-236, 2002.[7] Hacioglu, A. and Özkol, I., “Modified BLX-? : DoubleDirectional Alpha Method”, Proceedings of the SixteenthHACIOGLU, ÖZKOL9