Computational Investigation of Flow Separation over NACA 23024 Airfoil at 6 Million Free Stream Reynolds Number Using k-Epsilon Turbulence Model

Author:

Anil Kumar B.S.,Ramalingaiah ,Manjunath S.,Ganganna Rudresh

Publisher

Elsevier BV

Subject

General Medicine

Reference7 articles.

1. David Hartwanger et al. “3 D modeling of a Wind Turbine using CFD” NAFEMS Conference, United Kingdom, 2008.

2. Wind Turbine airfoil catalogue;Bertagnolio,2001

3. H.Gao et al. “Computational study of unsteady flows around dragonfly and smooth airfoils at low Reynolds number” 46th AIAA Aerospace sciences meeting and exhibit, Reno, Navada,, 2008.

4. Vance Dippold, III, “Investigation of Wall Function and Turbulence Model Performance within the Wind Code”, 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10–13 January 2005, Reno, Nevada.

5. S. Sarada, M.Shiva Shankar and Rudresh Ganganna “ Numerical simulation of Viscous, incompressible flow around NACA 64618 subsonic airfoil using Computational Fluid Dynamics”, Proceedings of National conference on advances in Mechanical Engineering, Allied Publishers Pvt Ltd, 2012.

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