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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| Hoofdauteurs: | , , , |
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| Formaat: | Artigo |
| Taal: | Inglês |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2019-03-01
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| Reeks: | INCAS Bulletin |
| Onderwerpen: | |
| Online toegang: | http://bulletin.incas.ro/files/dina_danaila_pricop_bunescu_vol_11_iss_1.pdf |
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