(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/920bb5u47wj...
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/do...)
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...)
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.
• ANSYS 12.1 (Part 1 of 3) ICEM CFD Hexa 2D ... )
4. Set solver and run simulation with Fluent
5. Results processing using Excel