Design a regenerator for a gas turbine engine. The engine is to deliver 50,000 hp with a compression ratio of 4:1 and a turbine inlet temperature of2,0000E The regenerator should have an effectiveness of 0.85 and pressure drops not to exceed 0.5 psi. The pressure drop of the combustor is 1.0 psi.
Our customer support team is here to answer your questions. Ask us anything!
👋 How can we help with you?