Influence of Camber Ratio and Thickness Ratio on the Airfoil Performance

Author:

Roy Sujit,Das Biplab,Biswas Agnimitra

Publisher

Springer Singapore

Reference20 articles.

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2. S. Hossain, M.F. Raiyan, M.N.U. Akanda, N.H. Jony, A comparative flow analysis of NACA 6409 and NACA 4412 aerofoil. Int. J. Res. Eng. Technol. 3(10), 342–350 (2014)

3. D.C. Eleni, T.I. Athanasios, M.P. Dionissios, Evaluation of the turbulence models for the simulation of the flow over a National Advisory Committee for Aeronautics (NACA) 0012 airfoil. J. Mech. Eng. Res. 4(3), 100–111 (2012)

4. M. Kevadiya, H.A. Vaidya, 2D analysis of NACA 4412 airfoil. Int. J. Innov. Res. Sci. Eng. Technol. 2(5), 1686–1691 (2013)

5. O. Gulzar, S. Gulzar, S. Bhatele, N. Soni, Impact of variation in angle of attack on NACA 7420 airfoil in transonic compressible flow using Spalart- Allmaras turbulence model. Int. J. Res. Mech. Eng. Technol. 4(2), 35–39 (2014)

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