A rotor ship $($see photo for reference$)$ has $1$ rotor, that is $4$ m in diameter, $25$ m tall, and rotates at $100$ rpm $.$ If the ship is moving $6\frac{m}{s}$ through still water and wind speed is $10\frac{m}{s}$ perpendicular to the ship's heading, calculate the net thrust generated by the rotor $($accounting for both lift and drag$).$ Use $1\mathrm{.}20k\frac{g}{m^3}$ for density of air.