6. High pressure air at 1360 K flows into an aircraft gas turbine and undergoes a...

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6. High pressure air at 1360 K flows into an aircraft gas turbine and undergoes a steady-state, steady-flow, adiabatic process to the turbine exit at 600 K. Calculate the work done per unit mass of air flowing through the turbine when (a) Temperature-dependent data are used. (b) Cp,ave at the average temperature is used. (c) Cp at 300 K is used. Hint: See Example 5-5 (15 pts) 6. High pressure air at 1360 K flows into an aircraft gas turbine and undergoes a steady-state, steady-flow, adiabatic process to the turbine exit at 600 K. Calculate the work done per unit mass of air flowing through the turbine when (a) Temperature-dependent data are used. (b) Cp,ave at the average temperature is used. (c) Cp at 300 K is used. Hint: See Example 5-5 (15 pts)