Computational Fluid Dynamics Analysis of Wind Turbine Blade at Various Angles of Attack and Different Reynolds Number

Author:

Patil Bhushan S.,Thakare Hitesh R.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference8 articles.

1. Schmitz F. W. (1967 Aerodynamics of the model airplane. Part I. Airfoil measurements, NACA TM X-60976.

2. Airfoil section characteristics at a low Reynolds number;Sunada;Journal of Fluids Engineering,1997

3. Comparison of wing characteristics at an ultralow Reynolds number;Sunada;Journal of Aircraft,2002

4. Nazmul Haque, Mohammad Ali, Ismat Ara, “Experimental investigation on the performance of NACA 4412 aerofoil with curved leading edge planform”, Procedia Engineering 105 (2015) 232-240, Elsevier.

5. Kroo I., Kunz P. J., (2000) Meso-scale ight and miniature rotorcraft development, Proceedings of the Conference on Fised, Flapping and Rotary ,Vehicles at very Low Reynolds Numbers, Univ. of Notre Dame, Notre Dame, IN, 184-196.

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