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;
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.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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