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CFD Analysis of Pressure Coefficient for NACA 4412

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Author(s): Mr. Mayurkymar kevadiya

Journal: International Journal of Engineering Trends and Technology
ISSN 2231-5381

Volume: 4;
Issue: 5;
Start page: 2041;
Date: 2013;
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Keywords: Computational fluid dynamics | Angle of Attack | Airfoil.

ABSTRACT
in this paper NACA 4412 airfoil profile is considered for analysis of wind turbine blade. Geometry of the airfoil is created using GAMBIT 2.4.6. And CFD analysis is carried out using FLUENT 6.3.26 at various angles of attack from 0˚ to 12˚. Variations of pressure coefficient are plotted in form of contour for 1 ×105 Reynolds number.
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