Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

The aim of this paper is to demonstrate the effects of the shape optimization on the missile performance at supersonic speeds. The N1G missile model shape variation, which decreased its aerodynamic drag and increased its aerodynamic lift at supersonic flow under determined constraints, was numerical...

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Bibliographic Details
Main Authors: Ahmet Şumnu, İbrahim Halil Güzelbey, Orkun Öğücü
Format: Article
Language:English
Published: Hindawi Limited 2020-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2020/1528435