The total wing drag is the sum of Cd_0 (drag due to shear stresses and pressure distributions on the airfoil) and the induced drag related to the efficiency of the load distribution and the wing tip vorticity.
Task: implement a way to assign the Cd_0 for a wing.
The total wing drag is the sum of Cd_0 (drag due to shear stresses and pressure distributions on the airfoil) and the induced drag related to the efficiency of the load distribution and the wing tip vorticity.
Task: implement a way to assign the Cd_0 for a wing.