GATE ME · 2017 · ME-1
Question 34: Applications
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Question 34
ME-1NAT2 marksNeeds review
The pressure ratio across a gas turbine (for air, specific heat at constant pressure,
J/kg. K and ratio of specific heats,
) is 10. If the inlet temperature to the turbine is 1200 K and the isentropic efficiency is 0.9, the gas temperature at turbine exit is ______ K.Log in to check the answer
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2017ME-1
GATE ME 2017 · Paper 1
Mechanical Engineering · Original paper archive
- Section
- Section ME-1
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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