The temperature and pressure at the inlet of a gas turbine are measured as 325 OC and 500kPa. The gas expands isentropically in the turbine and the pressure gets reduced to 150kPa at the exit. Determine the gas temperature at the exit after expansion. Heat is added at constant volume to increase the temperature of the gas to 300 OC to continue with the next cycle. Determine the heat added to the gas. Assume R=287 J/kg.K and Cp/Cv=1.4;

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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The temperature and pressure at the
inlet of a gas turbine are measured as
325 OC and 500kPa. The gas expands
isentropically in the turbine and the
pressure gets reduced to 150kPa at the
exit. Determine the gas temperature at
the exit after expansion. Heat is added at
constant volume to increase the
temperature of the gas to 300 OC to
continue with the next cycle. Determine
the heat added to the gas. Assume
R=287 J/kg.K and Cp/Cv=1.4;
Transcribed Image Text:The temperature and pressure at the inlet of a gas turbine are measured as 325 OC and 500kPa. The gas expands isentropically in the turbine and the pressure gets reduced to 150kPa at the exit. Determine the gas temperature at the exit after expansion. Heat is added at constant volume to increase the temperature of the gas to 300 OC to continue with the next cycle. Determine the heat added to the gas. Assume R=287 J/kg.K and Cp/Cv=1.4;
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