ANSYS Fluent: NACA 2412 airfoil with Angle of Attack Rotation and Varying Inlet velocity

The following video shows the ANSYS fluent procedure for NACA 2412 airfoil. the primary aim is to get the Coefficient of Lift and Coefficient of Drag values for varying Inlet velocity, but a constant Angle of attack, and, Varying angle of attack and a constant velocity. This project is being done using "Parameters set". Both the simulation can be done at once using Parameter sets.