Air flows isentropically through a converging nozzle attached to a large tank, where the absolute pressure is \(171 \mathrm{kPa}\) and the temperature is \(27^{\circ} \mathrm{C}\). At the inlet section the Mach number is 0.2 . The nozzle discharges to the atmosphere; the discharge area is \(0.015 \mathrm{~m}^{2}\). Determine the magnitude and direction of the force that must be applied to hold the nozzle in place.