- #1
roberto t
- 1
- 0
Hey Mech Eng Forum, I'm currently examining the performance on gas turbine and wondering:
How is the performance of gas turbines (Primarily thermal efficiency and net-work output) influenced by the pressure ratio and temperature constraints? Additionally, what is the benefit of 2 stage compression with intercooling?
Thanks!
How is the performance of gas turbines (Primarily thermal efficiency and net-work output) influenced by the pressure ratio and temperature constraints? Additionally, what is the benefit of 2 stage compression with intercooling?
Thanks!