1.

The pressure ratio across a gas turbine (for air, specific heat at constant pressure, cp=1040J/kgK and ratio of specifc heats γ=1.4 is 10. If the inlet temeprature to the turbine is 1200K and te isentropic efficiency is 0.9, the gas temperature at turbine exist is679.4

Answer» The pressure ratio across a gas turbine (for air, specific heat at constant pressure, cp=1040J/kgK and ratio of specifc heats γ=1.4 is 10. If the inlet temeprature to the turbine is 1200K and te isentropic efficiency is 0.9, the gas temperature at turbine exist is
  1. 679.4


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