Gas Turbine Thermodynamics Calculator

Performing calculation of a gas turbine thermodynamic cycle

The APP allows the user to perform a 0-D evaluation of a brayton cycle (gas turbine), starting from basic condition (such as inlet temperature, pressure ratio, etc.). You can choose to enable an inter-cooled compression and/or a post-combustion (with both the option the mid-pressure will be evaluated with a parameter K, ratio of the logarithm of low pressure ratio over the total pressure ratio).

All the pressure losses (inlet, combustion chamber and outlet) are evaluated as percentage of the absolute pressure.