(part 2 of 2) NACA airfoil CFD simulation

Easy and simple CFD analysis of incompressible flow over a airfoil is present. 720p HD resolution is recommended. Downloading supporting excel file https://www.dropbox.com/s/920bb5u47wjfj8r/airfoil.xlsx -part 1 of 2- 1. Get experimental data for comparison with CFD results. (you can download 'getdata' shareware from here. http://getdata-graph-digitizer.com/download.php) Experimental data was given by "Theory of Wing Sections" by IRA H.ABBOTT et al. 2. Create geometry with airfoil point coordinate data using ICEM-CFD. (Airfoil coordinate data was given by "UIUC Airfoil Database" http://aerospace.illinois.edu/m-selig/ads/coord_database.html) -part 2 of 2- 3. Creating blocking topology of airfoil and boundary domain and generate mesh using ICEM-CFD (y+ calculation was given by CFD-ONLINE http://www.cfd-online.com) (This topogoly is only for blunt trailing edge airfoil. If you have sharp trailing edge airfoil, ANSYS tutorial video should be better. http://youtu.be/tYrbScUH9RE) 4. Set solver and run simulation with Fluent 5. Results processing using Excel