دورية أكاديمية

Using genetic algorithms to optimize airfoils in incompressible regime

التفاصيل البيبلوغرافية
العنوان: Using genetic algorithms to optimize airfoils in incompressible regime
المؤلفون: Adrian DINA, Sterian DANAILA, Mihai-Victor PRICOP, Ionut BUNESCU
المصدر: INCAS Bulletin, Vol 11, Iss 1, Pp 79-90 (2019)
بيانات النشر: National Institute for Aerospace Research “Elie Carafoli” - INCAS, 2019.
سنة النشر: 2019
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: optimization, genetic algorithms, parametrization, XFOIL, aerodynamic models, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: 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 geometry is approximated by a parametrization, which enables to reduce the number of needed parameters to as few as possible, while effectively controlling the major aerodynamic features. The present work has been done on the Class-Shape function Transformation method (CST) [1, 2]. Also, the paper introduces the concept of Genetic Algorithm (GA) to optimize a NACA airfoil for specific conditions. A Matlab program has been developed to implement CS into the Global Optimization Toolkit. The pressure distribution lift and drag coefficients of the airfoil geometries have been calculated using two programs. The first one is an in-house code based on the Hess-Smith [3] panel technique and on the boundary layer integral equations, while the second is an XFOIL program. The optimized airfoil has improved aerodynamic characteristics as compared to the original one. The optimized airfoil is validated using the Ansys-Fluent commercial code.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 2066-8201
2247-4528
العلاقة: http://bulletin.incas.ro/files/dina_danaila_pricop_bunescu_vol_11_iss_1.pdfTest; https://doaj.org/toc/2066-8201Test; https://doaj.org/toc/2247-4528Test
DOI: 10.13111/2066-8201.2019.11.1.6
الوصول الحر: https://doaj.org/article/2e41cfe6d9b84cf5817608ffa6dfd1e5Test
رقم الانضمام: edsdoj.2e41cfe6d9b84cf5817608ffa6dfd1e5
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:20668201
22474528
DOI:10.13111/2066-8201.2019.11.1.6