An Ideal Gas, with a specific heat (Cp) of 1.01 kJ.kg-1.K-1, flows through a nozzle. The temperature of the gas at entry to the nozzle is 22oC, and its speed is very low (i.e. negligible). The gas temperature at exit from the nozzle is 8oC. Assuming steady-state, steady-flow (SSSF) operation, and that flow through the nozzle is adiabatic, calculate the speed of the gas (in m.s-1) at exit from the nozzle