Numerical Analysis of Joukowski (T = 12%) Airfoil by k-ε Turbulence Model at High Reynolds Number

Author:

Jain RaviORCID,Sheikh Mohd. YunusORCID,Singh DharmendraORCID,Tripathi ManojORCID

Publisher

Springer International Publishing

Reference16 articles.

1. Jain, R., Mohammad, U.: CFD approach of Joukowski airfoil (T = 12%), comparison of its aerodynamic performance with NACA airfoils using k-ε turbulence model with 3 million reynolds number. IRJET 5(10), 1414–1418 (2018)

2. Bhargava, V., Rao, Ch.K., Dwivedi, Y.D.: Pressure distribution & aerodynamic characteristics of NACA airfoils using computational panel method for 2D lifting flow. Int. J. Eng. Res. 5(11), 2347–5013 (2017)

3. He, W., Yu, P., Li, L.K.B.: Ground effects on the stability of separated flow around a NACA 4415 airfoil at low Reynolds numbers. Aerosp. Sci. Technol. 72, 63–76 (2018)

4. D’Souza, A.G., Concessao, J.I., Quadros, J.: Study of airfoil design parameters for low speed wind tunnel. J. Mech. Eng. Autom. 5(3B), 47–54 (2015)

5. Şahin, I., Acir, A.: Numerical and experimental investigations of lift and drag performances of NACA 0015 wind turbine airfoil. Int. J. Mater. Mech. Manuf. 3(1), 22–25 (2015)

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