Hi friends?
We have centaur 4500 and 4700 gas turbines from solat turbine inc. I want to know how to calculate the TRIT(Turbine rotor inlet temprature) while i measure T1, T2(Temprature of PCD) WA(Air flow) wf(fuel flow) Exhust temprature, exhust diffrential pressure.
The turbine is split shaft and axial 11 stage compressor.
Best regards