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

AERODYNAMIC ANALYSES OF NACA 63-215

Ümit Korkmaz(GAZİANTEP ÜNİVERSİTESİ, HAVACILIK VE UZAY BİLİMLERİ FAKÜLTESİ)0000-0001-6839-1587
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
Pages
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Publication Date
2020-10-16
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Also, flow separation was investigated at different AoA values.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this study, aerodynamic performance of NACA 63-215 airfoil was investigated.
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Key Findings & Data:Aerodynamic performance of the airfoils is changed with respect to angle of attack (AoA) values.
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Conclusion & Impact:Also, flow separation was investigated at different AoA values.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Airfoil · Aerodynamic · CFD

Abstract

In this study, aerodynamic performance of NACA 63-215 airfoil was investigated. Aerodynamic performance of the airfoils is changed with respect to angle of attack (AoA) values. The AoA increases, the separation of the boundary layers on the upper and lower surface of the wing increases. This situation is effect on the aerodynamic performance. So aerodynamic parameters (lift coeff. and drag coeff.) at different AoA values were investigated. Also, flow separation was investigated at different AoA values.

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Cite This Article

Korkmaz, Ü., Göv, İ., Doğru, M. H. (2020). AERODYNAMIC ANALYSES OF NACA 63-215. The International Journal of Energy and Engineering Sciences, Volume: 5 Issue: 2. https://ajindex.com/articles/1551727

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