This tutorial shows how to build and compute a CFD analysis of a NASA 0015 symmetric airfoil.   A velocity of 66 ft/s will be induced over the airfoil section and outputs of velocity profile, pressure distribution, and lift and drag forces will be calculated in the analysis. Enjoy! 

PLEASE NOTE:  As of the Abaqus 2017 release Abaqus/CFD is no longer available as a stand-alone product.  If you are interested in this technology, please check out our CFD capabilities on the 3DEXPERIENCE Platform.