model with k= 5/3. Ignore the effects of motion and gravity. Let T,=20 °C, Po=1 bar a) What are the possible turbine exit temperatures? Report a range in K. Determine the power developed and exergy destroyed (in kW) for the minimum turbine b) exit temperature. c) Determine the power developed and exergy destroyed (in kW) for the maximum turbine exit temperature. Plot each of the following versus the turbine exit temperature, in K. d) The power developed, in kW. e) The rate of exergy destruction in the turbine, in kW. 6The exergetic turbine efficiency, as a percentage.
model with k= 5/3. Ignore the effects of motion and gravity. Let T,=20 °C, Po=1 bar a) What are the possible turbine exit temperatures? Report a range in K. Determine the power developed and exergy destroyed (in kW) for the minimum turbine b) exit temperature. c) Determine the power developed and exergy destroyed (in kW) for the maximum turbine exit temperature. Plot each of the following versus the turbine exit temperature, in K. d) The power developed, in kW. e) The rate of exergy destruction in the turbine, in kW. 6The exergetic turbine efficiency, as a percentage.
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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![ADJUST
7.118 Argon enters an insulated turbine operating at steady state at 1000°C and 2 MPa
and exhausts at 400 kPa. The mass flow rate is 0.75 kg/s. For argon, use the ideal gas
model with k = 5/3. Ignore the effects of motion and gravity. Let T=20 °C, Po=1 bar
a) Whạt are the possible turbine exit temperatures? Report a range in K.
b) Determine the power developed and exergy destroyed (in kW) for the minimum turbine
exit temperature.
c) Determine the power developed and exergy destroyed (in kW) for the maximum
turbine exit temperature.
Plot each of the following versus the turbine exit temperature, in K.
d)
e) The rate of exergy destruction in the turbine, in kW.
(O The exergetic turbine efficiency, as a percentage.
The power developed, in kW.
AUTO
Cancel
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Transcribed Image Text:ADJUST
7.118 Argon enters an insulated turbine operating at steady state at 1000°C and 2 MPa
and exhausts at 400 kPa. The mass flow rate is 0.75 kg/s. For argon, use the ideal gas
model with k = 5/3. Ignore the effects of motion and gravity. Let T=20 °C, Po=1 bar
a) Whạt are the possible turbine exit temperatures? Report a range in K.
b) Determine the power developed and exergy destroyed (in kW) for the minimum turbine
exit temperature.
c) Determine the power developed and exergy destroyed (in kW) for the maximum
turbine exit temperature.
Plot each of the following versus the turbine exit temperature, in K.
d)
e) The rate of exergy destruction in the turbine, in kW.
(O The exergetic turbine efficiency, as a percentage.
The power developed, in kW.
AUTO
Cancel
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