NACA Airfoil – Geometry and Mesh download

NACA refers to the National Advisory Committee for Aeronautics that was founded in 1915 in the Unites states of America which supported research and the industrialisation of  aerospace engineering. The geometry in this section was used in my Youtube tutorial video for simulating the aerodynamics around an NACA airfoil.

To download the geometry, please click below:

+Download Geometry

To download the Mesh file, please click below:

+Download Mesh File

The picture below shows the final result of a steady state CFD simulation on the same airfoil using the Spalart Allmaras 1 equation turbulent model

Velocity contour around the airfoil
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