3. A gas turbine uses the Joule cycle. The inlet pressure and temperature to the compressor are respectively 1 bar and -10°C. After constant pressure heating, the pressure and temperature are 7 bar and 700°C respectively. The flow rate of air is 0.4 kg/s. Calculate the following. 1. The cycle efficiency. 2. The heat transfer into the heater. 3. the net power output. y= 1.4 Cp = 1.005 kJ/kg K %3D
3. A gas turbine uses the Joule cycle. The inlet pressure and temperature to the compressor are respectively 1 bar and -10°C. After constant pressure heating, the pressure and temperature are 7 bar and 700°C respectively. The flow rate of air is 0.4 kg/s. Calculate the following. 1. The cycle efficiency. 2. The heat transfer into the heater. 3. the net power output. y= 1.4 Cp = 1.005 kJ/kg K %3D
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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![3. A gas turbine uses the Joule cycle. The inlet pressure and temperature to the compressor are
respectively 1 bar and -10°C. After constant pressure heating, the pressure and temperature are 7
bar and 700°C respectively. The flow rate of air is 0.4 kg/s.
Calculate the following. 1. The cycle efficiency. 2. The heat transfer into the heater. 3. the net
power output. y= 1.4 Cp = 1.005 kJ/kg K
%3D](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F5aebdc8d-6927-4cfa-bc36-b84f4a7d9d18%2F0aae5ede-d4a2-4bf4-99fc-2ca444a1c99b%2Faawd57_processed.jpeg&w=3840&q=75)
Transcribed Image Text:3. A gas turbine uses the Joule cycle. The inlet pressure and temperature to the compressor are
respectively 1 bar and -10°C. After constant pressure heating, the pressure and temperature are 7
bar and 700°C respectively. The flow rate of air is 0.4 kg/s.
Calculate the following. 1. The cycle efficiency. 2. The heat transfer into the heater. 3. the net
power output. y= 1.4 Cp = 1.005 kJ/kg K
%3D
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