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The compressor and turbine unit of a small gas turbine plant have an isentropic efficiency of 88%. The inlet air temp. of compressor is at $200^0C$ and maximum temp.
written 7.7 years ago by | • modified 2.7 years ago |
during the cycle is limited to $750^0C$. The pressure ratio is 4. Calculate specific output, overall efficiency of cycle. Take γ=1.4 and neglect all losses.
Mumbai University > Mechanical Engineering > Sem 7 > Power Plant Engineering
Marks : 10M
Year: Dec 2015
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