An ideal gas enters a turbine with a velocity of 40 m/s through an inlet pipe with a diameter of 160 mm. The ideal gas enters the turbine at a temperature of 660°C and a pressure of 800 kPa. The ideal gas leaves the turbine with a velocity of 150 m/s through an outlet pipe with a diameter of 100 mm. The power output from the turbine is 350 kW. The heat lost from the turbine to the surrounding amounts to 6% of the power output from the turbine. Changes in kinetic energy and potential energy can be neglected. For the ideal gas, use R = 0.287 kJ/kg.K and c, = 1.11 kJ/kg.K| i) Sketch the system/control volume for the above problem Show the boundary/control surface and energy interactions clearly in the sketch. 11) Determine the mass flow rate of the ideal gas, kg/s. i11) Determine the temperature of the ideal gas leaving the turbine, °C. iv) Determine the pressure of the ideal gas leaving the turbine, kPa. v) Suggest one way to increase the power output from the turbine.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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An ideal gas enters a turbine with a velocity of 40 m/s through an inlet pipe with a diameter
of 160 mm. The ideal gas enters the turbine at a temperature of 660°C and a pressure of
800 kPa. The ideal gas leaves the turbine with a velocity of 150 m/s through an outlet pipe
with a diameter of 100 mm. The power output from the turbine is 350 kW. The heat lost
from the turbine to the surrounding amounts to 6% of the power output from the turbine.
Changes in kinetic energy and potential energy can be neglected.
For the ideal gas, use R = 0.287 kJ/kg.K and c, = 1.11 kJ/kg.K|
i) Sketch the system/control volume for the above problem Show the
boundary/control surface and energy interactions clearly in the sketch.
11) Determine the mass flow rate of the ideal gas, kg/s.
i11) Determine the temperature of the ideal gas leaving the turbine, °C.
iv) Determine the pressure of the ideal gas leaving the turbine, kPa.
v) Suggest one way to increase the power output from the turbine.
Transcribed Image Text:An ideal gas enters a turbine with a velocity of 40 m/s through an inlet pipe with a diameter of 160 mm. The ideal gas enters the turbine at a temperature of 660°C and a pressure of 800 kPa. The ideal gas leaves the turbine with a velocity of 150 m/s through an outlet pipe with a diameter of 100 mm. The power output from the turbine is 350 kW. The heat lost from the turbine to the surrounding amounts to 6% of the power output from the turbine. Changes in kinetic energy and potential energy can be neglected. For the ideal gas, use R = 0.287 kJ/kg.K and c, = 1.11 kJ/kg.K| i) Sketch the system/control volume for the above problem Show the boundary/control surface and energy interactions clearly in the sketch. 11) Determine the mass flow rate of the ideal gas, kg/s. i11) Determine the temperature of the ideal gas leaving the turbine, °C. iv) Determine the pressure of the ideal gas leaving the turbine, kPa. v) Suggest one way to increase the power output from the turbine.
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