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Dergiler / The International Journal of Energy and Engineering Sciences / 2020 / Volume: 5 Issue: 2

AERODYNAMIC OPTIMIZATION OF NACA 0012 AIRFOIL

İbrahim Göv(GAZİANTEP ÜNİVERSİTESİ, HAVACILIK VE UZAY BİLİMLERİ FAKÜLTESİ)0000-0002-5513-0158
Mehmet Hanifi Doğru(GAZİANTEP ÜNİVERSİTESİ, HAVACILIK VE UZAY BİLİMLERİ FAKÜLTESİ)0000-0001-6038-8308
Sayfa
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Yayın Tarihi
2020-10-16
DOI
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⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

Commonly used NACA 0012 Airfoil is optimized at different angle of attack values using a commercial CFD program ANSYS.

📌 3 Maddede Bu Makale

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Amaç & Hipotez:Airfoils are used to produce lift force to carrying the weight of the aircrafts.
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Temel Bulgular & Veri:Hence, airfoil shape is directly affecting the aerodynamic performance of the wings.
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Sonuç & Katkı:Commonly used NACA 0012 Airfoil is optimized at different angle of attack values using a commercial CFD program ANSYS.
🔬Tür:Modelleme & Sayısal Simülasyon
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:CFD · Optimization · Aerodynamic

Abstract

Airfoils are used to produce lift force to carrying the weight of the aircrafts. Aerodynamic forces are directly related to airfoil shape. The force parallel to the direction of relative motion is defined as drag, and the force perpendicular to the direction of movement is defined as lift. Hence, airfoil shape is directly affecting the aerodynamic performance of the wings. In this study, aerodynamic optimization of an airfoil is performed using computational fluid dynamic (CFD) analysis to increase the aerodynamic performance of the wings. Commonly used NACA 0012 Airfoil is optimized at different angle of attack values using a commercial CFD program ANSYS.

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Bu Makaleye Atıf Yap

Göv, İ., Doğru, M. H. (2020). AERODYNAMIC OPTIMIZATION OF NACA 0012 AIRFOIL. The International Journal of Energy and Engineering Sciences, Volume: 5 Issue: 2. https://ajindex.com/articles/1551726

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Kaynakça (10)

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