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A simulation regarding analysis of specific NACA airfoils under conditions of mainly Re 5e5 & M 0.1

Análise da Asa Delta com análise do perfil NACA 4412

-project to analyse flow pattern for a NACA duct in a flat plate

NACA 0012 airfoil from NASA's TMR website.

This project has expanded a bit to include the following:
-Result validation of NACA0012
-icing of NACA0012
-Turbulence model comparison (LES and RANS) for NACA0012

CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees.

Reference:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf

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