The discussion centers on calculating the turbine inlet temperature (TIT) for gas turbines using specific parameters such as fuel flow, compressor discharge temperatures, and the lower heating value (LHV) of fuel. Participants recommend utilizing NASA's Chemical Equilibrium with Applications (CEA) code, which is freely available and provides accurate estimations for TIT. Additionally, a technical document from GE Power offers valuable data on firing temperatures, serving as a reference for target values.
PREREQUISITESEngineers, thermodynamic analysts, and professionals involved in gas turbine design and optimization will benefit from this discussion.