CFD ANALYSIS OF STATIC PRESSURE AND DYNAMIC PRESSURE FOR NACA 4412
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International Journal of Engineering Trends and Technology (IJETT) | 
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| © 2013 by IJETT Journal | ||
| Volume-4 Issue-8 |
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| Year of Publication : 2013 | ||
| Authors : Mr. Arvind Prabhakar |
Citation
Mr. Arvind Prabhakar. "CFD ANALYSIS OF STATIC PRESSURE AND DYNAMIC PRESSURE FOR NACA 4412". International Journal of Engineering Trends and Technology (IJETT). V4(8):3258-3265 Jul 2013. ISSN:2231-5381. www.ijettjournal.org. published by seventh sense research group.
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 And CFD analysis is carried out using commercial code ANSYS 13.0 FLUENT at an inlet boundary condition of V sound (i.e. 340.29 m/s) for angles of attack of 0 ?, 6, 12 AND 16 ?. Standard k - ? turbulence model with standard wall function is used for analysis. Variations of static pressure and dynamic pressure are plotted in form of contour.
References
i. http://en.wikipedia.org/wiki/Static_pressure
ii. http://en.wikipedia.org/wiki/Dynamic_pressure
iii. http://kgraham.eng.ua.edu/classes/AEM314/lecture_notes /airfoil_nomenclature.pdf
iv. http://www.ijettjournal.org/volume - 4/issue - 5/IJETT - V4I5P142.pdf
v. ‘Flight Theory and Aerodynamics: A Practical Guide for Operational Safety’ By Charles E. Dole, James E. Lewis
vi. http://flightmechanics.blogspot.in/2010/10/stagnation - point.html
Keywords
computational fluid dynamics, angle of attack (AOA) , airfoil , Vsound