V is the freestream fluid velocity, typically the true airspeed of the aircraft or the water speed of the vessel
n is the rotational speed of the propeller in revolutions per unit of time
D is the propeller's diameter
Why in my aerodynamic book from aeronautics university write V/n in advance ratio formula is aerodynamic /"effective" pitch(I agree with that), but some members which are aerodynamics experts at this site said that this is geometric pitch(zero slip)?
example