Right option is (c) J=\(\frac{V}{nD}\)
For explanation I would say: The propeller efficiency depends on the propeller advance ratio and power coefficient. Propeller advance ratio is given by J=\(\frac{V}{nD}\) where J is propeller advance ratio, V is true airspeed, n is rotational speed and D is propeller diameter. Also the pressure coefficient is given by CP=\(\frac{P}{\frac{\rho n^3D^5}{2}}\) where CP is pressure coefficient, ρ is density, P is shaft power, n is rotational speed and D is propeller diameter.