CFD ANALYSIS OF STATIC PRESSURE AND DYNAMIC PRESSURE FOR NACA 4412

  ijett-book-cover  International Journal of Engineering Trends and Technology (IJETT)          
  
© 2013 by IJETT Journal
Volume-4 Issue-8                      
Year of Publication : 2013
Authors : Mr. Arvind Prabhakar

MLA 

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 - ε 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