Air flows steadily from a tank, through a hose of diameter D=0.04 m, and exits to the atmosphere from a nozzle of diameter d=0.015 m as shown in the figure below. The gage pressure in the tank remains constant at 6 kPa and the atmospheric conditions are standard temperature and pressure. Consider air density of 1.2 kg/m. (a) Determine the flowrate, Q. (b) Determine the pressure in the hose, p2. P (1) Air (2) (3)