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NACA 2412 Airfoil

NACA 2412 Airfoil

grabcad

This is a NACA 2412 airfoil with a 1.1m chord. The model is set up for fluid flow calculations. I used Ansys-Fluent v13 to calculate pressures, velocities, lift, etc. Screenshots are from Fluent and are for mach number, M=0.1 (~34 m/s), inviscid, incompressible flow. I also attached a screenshot of static pressure with flow moving at Mach 0.8 using viscous, compressible flow characteristics.

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