loop gas turbine. The mixture enters the turbine at 0.8 MPa and 1527 °C and expands isentropically to a pressure of 700 kPa, using table A.1 and Table A2. c, determine the mass flow rate(kg/s) of the gas mixture needed to produce1.36 MW when the inlet conditions for velocity and height are is 660 m/s and 200 m respectively, and exit conditions are at 90 m/s and 5 m, assume no heat loss and a value of 1.443 for the heat capacity ratio of the gas mixture.
Fig: 1