Questions › Category: Compressors Gas Turbines and Jet Engines › The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio 0 Vote Up Vote Down VideRime Staff asked 3 years ago The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio (A) Increases (Ans) (B) Decreases (C) First increases and then decreases (D) First decreases and then increases Share this Now with Friends: Share on WhatsApp (Opens in new window) WhatsApp Share on Telegram (Opens in new window) Telegram More Related