(5). The compressor of an open-cycle gas turbine unit receives air at 100kPa, 18°C and delivers it at 400kPa, 200°C to the combustion chamber, where the temperature is raised at constant pressure to 650°C. The hot gases pass through the turbine having an isentropic efficiency of 85% and exhaust of 100kPa. Calculate: (a). the isentropic efficiency of the compressor (b). the net work per kg of air For air: For gas: Y = 1.4 Y = 1.333 ©p= I.005kJ/kgK = = 1.150kJ/kgK

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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(5). The compressor of an open-cycle gas turbine unit receives air at 100kPa,
18°C and delivers it at 400kPa, 200°C to the combustion chamber, where the
temperature is raised at constant pressure to 650°C. The hot gases pass
through the turbine having an isentropic efficiency of 85% and exhaust of
100kPa. Calculate:
(a). the isentropic efficiency of the compressor
(b). the net work per kg of air
For air:
For gas:
Y = 1.4
Y = 1.333
€p= I.005kJ/kgK
C₂ = 1.150kJ/kgK
Transcribed Image Text:(5). The compressor of an open-cycle gas turbine unit receives air at 100kPa, 18°C and delivers it at 400kPa, 200°C to the combustion chamber, where the temperature is raised at constant pressure to 650°C. The hot gases pass through the turbine having an isentropic efficiency of 85% and exhaust of 100kPa. Calculate: (a). the isentropic efficiency of the compressor (b). the net work per kg of air For air: For gas: Y = 1.4 Y = 1.333 €p= I.005kJ/kgK C₂ = 1.150kJ/kgK
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