The following is a schematic of a gas turbine for aircraft propulsion. Assume there's no heat loss from the system and there's no discernible change in potential energy. Find th exit velocity of air out of the propulsion system, i.e. Vs. Hnt: Take one compartment at a time and proceed accordingly. Pay attention to the initial and final states for each of these systems and the sign convention. W=1000 kJ Q=5000 kJ Compressor Comustors Turbine V.-10 m/s; h.-30 kJ/kg Product V=?: h 30 kJ/kg Air in W-1000 kJ V,-0 m/s: hANozzle hy h2 Gas generator Diffuser V,-0 m/s; h, Mass flow rate 10 kg/s throughout the system