Using genetic algorithms to optimize airfoils in incompressible regime

Using genetic algorithms to optimize airfoils in incompressible regime

Aerodynamic optimization is a very actual problem in aircraft design and airfoils are basic two-dimensional shape forming cross sections of wings. Traditionally, the airfoil geometry if defined by a very large number of coordinates. Nowadays, in order to simplify the optimization, the airfoil geomet...

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Bibliographic Details
Main Authors:	Adrian DINA, Sterian DANAILA, Mihai-Victor PRICOP, Ionut BUNESCU
Format:	Article
Language:	English
Published:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2019-03-01
Series:	INCAS Bulletin
Subjects:	optimization genetic algorithms parametrization XFOIL aerodynamic models
Online Access:	http://bulletin.incas.ro/files/dina_danaila_pricop_bunescu_vol_11_iss_1.pdf

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