NACA2412 Tutorial in ANSYS Fluent (Student Version) - Lift, Drag, Angle of Attack

In this tutorial I will conduct the analysis of a NACA2412 Airfoil using ANSYS fluent student version. I will also show how to change the angle of attack of the airfoil, and how that affects the simulation & results. 00:00 - 00:53 - Intro 00:53 - 5:30 - Creating Airfoil Curve File 5:30 - 15:02 - Creating Geometry: Airfoil import & C type domain 15:02 - 16:48 - How to save ANSYS files 16:48 - 22:03 - Meshing 22:03 - 27:13 - Y+ check 28:23 -33:24 - Simulation set up 33:24 - 34:58 - Solving 34:58 - 39:45 - Comparison with experimental data 39:45 - 44:20 - Plotting results 44:20 - 52:03 - Changing angle of attack 52:03- 53:20 - Plotting y+ 53:20 Outro Video mentioned by Anthony T that helped with mesh sizing: https://www.youtube.com/watch?v=nzvEvLCxOss&t=1050s Experimental data: https://ntrs.nasa.gov/citations/19930090976 For enquiries: [email protected]