Analysis of NACA Airfoil | CFD Vs Experimental | Ansys Fluent Simulation | Xdynemo

This video is about finding out the lift force generated by NACA 2412 Airfoil using ANSYS Fluent workbench. The results from CFD are compared with the wind tunnel experimental data to calculate the error in the CFD results. This video serves as a tutorial to import Airfoil coordinates file to ANSYS and performing Meshing, Choosing Solver settings, generating lift force reports and pressure contours in ANSYS workbench. Download NACA Data File here