This project is about Bryton Cycle (the basic cycle for Gas Turbine engine) Consider a gas turbine engine that operates on the basis of Bryton cycle. The isentropic efficiency of the turbine and compressor is 85% and 80%, respectively. The air flow rate is 40 kg/s Use the EES software to do the performance analysis of the cycle according to the following description: The pressure at the inlet and exit of the turbine are 1500 kPa and 100 kPa, respectively. Ignore pressure loss due to friction in heat exchangers. Change the temperature at the inlet of the turbine different times (repeat the caclulations at least 4 times by changing inlet turbine temperature in a range from 800 oC to 1300 oC). 1- 2- 3- For the above conditions calculate: The power input to the compressor and power output form the turbine. The rate of heat input and output to the cycle. The thermal efficiency of the cycle. The rate of exergy destruction for each component in the cycle .The total rate of exergy destruction of the whole cycle and the percentage of that exergy loss in each component. The second law efficiency of the cycle. PLOT all the above results as a function of the pressure ratio. This project is about Bryton Cycle (the basic cycle for Gas Turbine engine) Consider a gas turbine engine that operates on the basis of Bryton cycle. The isentropic efficiency of the turbine and compressor is 85% and 80%, respectively. The air flow rate is 40 kg/s Use the EES software to do the performance analysis of the cycle according to the following description: The pressure at the inlet and exit of the turbine are 1500 kPa and 100 kPa, respectively. Ignore pressure loss due to friction in heat exchangers. Change the temperature at the inlet of the turbine different times (repeat the caclulations at least 4 times by changing inlet turbine temperature in a range from 800 oC to 1300 oC). 1- 2- 3- For the above conditions calculate: The power input to the compressor and power output form the turbine. The rate of heat input and output to the cycle. The thermal efficiency of the cycle. The rate of exergy destruction for each component in the cycle .The total rate of exergy destruction of the whole cycle and the percentage of that exergy loss in each component. The second law efficiency of the cycle. PLOT all the above results as a function of the pressure ratio