Q2. A gas turbine with air as the working fluid has two ideal turbine sections, the first of which drives the ideal compressor, with the second producing the power output. The compressor input is at 290 K, 100 kPa, and the exit is at 450 kPa. A fraction of flow, x, bypasses the burner and the rest goes through the burner where 1200 kJ/kg is added by combustion. The two flows then mix before entering the first turbine and continue through the second turbine, with exhaust at 100 kPa. If the mixing should result in a temperature of 1000 K into the first turbine find the fraction x. Find the required pressure and temperature into the second turbine and its specific power output. Take C,-1.004 and 1.13 kJ/kg.K for cold and hot air respectively.
Q2. A gas turbine with air as the working fluid has two ideal turbine sections, the first of which drives the ideal compressor, with the second producing the power output. The compressor input is at 290 K, 100 kPa, and the exit is at 450 kPa. A fraction of flow, x, bypasses the burner and the rest goes through the burner where 1200 kJ/kg is added by combustion. The two flows then mix before entering the first turbine and continue through the second turbine, with exhaust at 100 kPa. If the mixing should result in a temperature of 1000 K into the first turbine find the fraction x. Find the required pressure and temperature into the second turbine and its specific power output. Take C,-1.004 and 1.13 kJ/kg.K for cold and hot air respectively.
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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Transcribed Image Text:Q2. A gas turbine with air as the working fluid has two ideal turbine sections, the first of
which drives the ideal compressor, with the second producing the power output. The
compressor input is at 290 K, 100 kPa, and the exit is at 450 kPa. A fraction of flow, x,
bypasses the burner and the rest goes through the burner where 1200 kJ/kg is added
by combustion. The two flows then mix before entering the first turbine and continue
through the second turbine, with exhaust at 100 kPa. If the mixing should result in a
temperature of 1000 K into the first turbine find the fraction x. Find the required
pressure and temperature into the second turbine and its specific power output. Take
C,=1.004 and 1.13 kJ/kg.K for cold and hot air respectively.
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