I assume you might be modelling a single blade of your propeller, since you want to calculate Lift?
If this is the case, you can simply orient your blade geometry such that the inflow direction is in, lets say, the [X+] direction. The Lift would now be the Forces in the [Z+] direction, i.e. Pressure Force Z + Viscous Force Z and the drag would be Pressure Force X + Viscous Force X.
The values of Pressure and Viscous forces can be derived by setting up a force plot in Result Control.
Please let me know if this helps