How to Use Parameters in Ansys Fluent to Create a Coefficient of Lift vs Alpha Graph

In this video, I show you how to use airfoiltools, Excel, SolidWorks, Spaceclaim, and Ansys Fluent to create a Coefficient of Lift vs Angle of Attack(Alpha) Graph. This exercise will teach you how to use parameters to test a NACA N2414-il airfoil at many different angles of attack. If you have any suggestions or recommendations for future videos, please leave them in the comments below. Chapters: 0:13 - Getting the coordinates for the airfoil curve 1:20 - Editing the CSV file 2:57 - Creating the airfoil CAD in SolidWorks 4:50 - Cleaning the airfoil CAD in Spaceclaim 6:39 - Setting up the flow domain geometry in Design Modeler 13:29 - Setting up the mesh 16:20 - Using the Reynold Number to calculate the inlet velocity 18:02 - Setting up the Fluent simulation 20:13 - Setting up the parameter sweep 21:23 - Creating the Coefficient of Lift vs Alpha graph and comparing to airfoiltools