The turbine of an aircraft uses 100kg/s of fuel to perform a flight speed and generates gases at its exit. The air inlet speed of this turbine is 100 m/s. In this system, we know that rhoAR = 1.2kg/m^3 , rhoGASES = 0.8kg/m^3 and that the turbine has its dimensions according to the figure below. From the information given, what is the velocity of the gases generated at the exit?
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