ANSYS 17.0 Fluent CFD - 3D Airfoil Tutorial

New tutorial in Ansys 17.0 Fluent CFD of a 3D NACA 2412 using dynamically changing velocity profile along with changing angle of attack. Velocity goes from 0 to 40m/s and the angle of attack from 0deg to 40deg. We will use turbulence flow models, generate CD and CL profiles, force results and generate pressure and velocity contour plots. We will be making fancy 3D videos in CFD-POST, using streamlines, volumetric rendering, specular lighting, etc. Files for download: 1) NACA Airfoil DATA: