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CFD ANALYSIS OF STATIC PRESSURE AND DYNAMIC PRESSURE FOR NACA 4412

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Author(s): Mr. Arvind Prabhakar,

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

Volume: 4;
Issue: 8;
Start page: 3258;
Date: 2013;
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Keywords: computational fluid dynamics | angle of attack (AOA) | airfoil | Vsound

ABSTRACT
The static pressure and dynamic pressure are important parameters and have a strong influence on airplane wing lift and stagnation point. In this paper NACA 4412 airfoil profile is considered for analysis of an airplane wing .The NACA 4412 airfoil is created using CATIA V5 AndCFD analysis is carried out using commercial code ANSYS 13.0 FLUENT at an inlet boundary condition of Vsound (i.e. 340.29 m/s) for angles of attack of 0˚, 6, 12 AND 16˚. Standard k-ε turbulence model with standard wall function is used for analysis. Variations of static pressure and dynamic pressure are plotted in form of contour.
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