Araştırma Makalesi
Yıl 2020,
Cilt: 5 Sayı: 2, 146 - 155, 16.10.2020
Öz
Kaynakça
- Chitte P., Jadhav P.K., Bansode S.S., 2013. Statistic and dynamic analysis of typical wing structure of aircraft using Nastran. International Journal of Application or Innovation in Engineering & Management (IJAIEM) 2, 7.
- Holst T. L., 1994. Computational Fluid Dynamics Uses in Fluid Dynamics/Aerodynamics Education. NASA Technical Memorandum 108834.
- Kavya G., Reddy B.C.R., 2015. Design and Finite Element Analysis of Aircraft Wing Using Ribs and Spars. International Journal & Magazine of Engineering Technology, Management and Research. 2, 11.
- Kumar B. S. A., Ramalingaiah, Manjunath S., Ganganna R., 2015. Computational Investigation of Flow Separation over Naca 23024 Airfoil at 6 Million Free Stream Reynolds Number. International Journal of Science, Technology and Society 3,6.
- Patel K.S., Patel S. B., Patel U. B., Ahuja A. P., 2014. CFD Analysis of an Aerofoil. International Journal of Engineering Research 3,3.
- Triet N.M., Viet N.N., Thang P. M., 2015. Aerodynamic Analysis of Aircraft Wing. VNU Journal of Science: Mathematics – Physics 31,2.
- Göv İ. and Korkmaz Ü., 2016. Comparison of Aerodynamic Performance of NACA 4412 and S809 Airfoil Profile. International Mechanical Engineering and Technologies Conference.
- Doğru, M. H. 2017. Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles. Çukurova University Journal of the Faculty of Engineering and Architecture, 32(3), 39-46.
- Göv, I., Dogru, M. H., & Korkmaz, U. 2019. Improvement of the aerodynamic performance of NACA 4412 using the adjustable airfoil profile during the flight. Journal of The Faculty of Engineering and Architecture of Gazi University, 34(2), 1110-1125.
- url: https://en.wikipedia.org/wiki/Adjoint_equation.
Yıl 2020,
Cilt: 5 Sayı: 2, 146 - 155, 16.10.2020
Öz
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.
Anahtar Kelimeler
Kaynakça
- Chitte P., Jadhav P.K., Bansode S.S., 2013. Statistic and dynamic analysis of typical wing structure of aircraft using Nastran. International Journal of Application or Innovation in Engineering & Management (IJAIEM) 2, 7.
- Holst T. L., 1994. Computational Fluid Dynamics Uses in Fluid Dynamics/Aerodynamics Education. NASA Technical Memorandum 108834.
- Kavya G., Reddy B.C.R., 2015. Design and Finite Element Analysis of Aircraft Wing Using Ribs and Spars. International Journal & Magazine of Engineering Technology, Management and Research. 2, 11.
- Kumar B. S. A., Ramalingaiah, Manjunath S., Ganganna R., 2015. Computational Investigation of Flow Separation over Naca 23024 Airfoil at 6 Million Free Stream Reynolds Number. International Journal of Science, Technology and Society 3,6.
- Patel K.S., Patel S. B., Patel U. B., Ahuja A. P., 2014. CFD Analysis of an Aerofoil. International Journal of Engineering Research 3,3.
- Triet N.M., Viet N.N., Thang P. M., 2015. Aerodynamic Analysis of Aircraft Wing. VNU Journal of Science: Mathematics – Physics 31,2.
- Göv İ. and Korkmaz Ü., 2016. Comparison of Aerodynamic Performance of NACA 4412 and S809 Airfoil Profile. International Mechanical Engineering and Technologies Conference.
- Doğru, M. H. 2017. Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles. Çukurova University Journal of the Faculty of Engineering and Architecture, 32(3), 39-46.
- Göv, I., Dogru, M. H., & Korkmaz, U. 2019. Improvement of the aerodynamic performance of NACA 4412 using the adjustable airfoil profile during the flight. Journal of The Faculty of Engineering and Architecture of Gazi University, 34(2), 1110-1125.
- url: https://en.wikipedia.org/wiki/Adjoint_equation.
Toplam 10 adet kaynakça vardır.
Ayrıntılar
| Birincil Dil | İngilizce |
|---|---|
| Bölüm | Research Article |
| Yazarlar | |
| Yayımlanma Tarihi | 16 Ekim 2020 |
| Kabul Tarihi | 14 Ekim 2020 |
| Yayımlandığı Sayı | Yıl 2020 Cilt: 5 Sayı: 2 |
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