- 07/13/2019 at 9:31 pm #1440227EduGorillaKeymasterSelect Question Language :
The Pressure ratio across a gas turbine (for air, specific heat at constant pressure, and ratio of specific heats, is 10. If the inlet temperature to the turbine is 1200K and the isentropic efficiency is 0.9, the gas temperature at turbine exit is ______ K.
Options :-Post your Training /Course EnquiryAre You looking institutes / coaching center for
- IIT-JEE, NEET, CAT
- Bank PO, SSC, Railways
- Study Abroad