Aerodynamic Investigation Of Flow Parameter Over Naca 4415 Airfoil By Computational Fluid Dynamics

Research Article
Pankaj Garg and Neelesh Soni
DOI: 
xxx-xxxxx-xxxx
Subject: 
science
KeyWords: 
Aerodynamics Airfoil, NACA 4415, Reynolds number, Angle of attack, lift, drag
Abstract: 

In this paper CFD analysis of NACA 4415 airfoil has been analyzed with the fluent software 6.3.26. During the CFD analysis the angle attack was taken 12 number was selected 1000000 and 1500000. It was found that increase of angle of attack, but after 160 come this situation. The Reynolds number was varied but no significant change was notice.

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