A gas turbine cycle has two stages of compression, each stage has an isentropic efficiency of 82%, with an intercooler between the stages. Air enters the first stage at 100 kPa, 24°C. Air exits the intercooler at 70°C. The maximum cycle temperature is 1250°C, and the cycle has a single turbine stage with pressure ratio of 23 and isentropic efficiency of 90%. The cycle also includes a regenerator with an effectiveness of 78%. Calculate the following
A gas turbine cycle has two stages of compression, each stage has an isentropic efficiency of 82%, with an intercooler between the stages. Air enters the first stage at 100 kPa, 24°C. Air exits the intercooler at 70°C. The maximum cycle temperature is 1250°C, and the cycle has a single turbine stage with pressure ratio of 23 and isentropic efficiency of 90%. The cycle also includes a regenerator with an effectiveness of 78%. Calculate the following
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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![A gas turbine cycle has two stages of
compression, each stage has an isentropic
efficiency of 82%, with an intercooler between
the stages. Air enters the first stage at 100
kPa, 24 C. Air exits the intercooler at 70 C. The
maximum cycle temperature is 1250 C, and
the cycle has a single turbine stage with
pressure ratio of 23 and isentropic efficiency of
90%. The cycle also includes a regenerator
with an effectiveness of 78%. Calculate the
following
Thermal Input heat Compressor
efficiency
Turbine
work
work](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F2d596f6a-32a2-493e-917d-5e9b7dec7c3c%2F715b9d6c-099b-4b5a-a2a3-944a04e09d0e%2Fjbvtf4f_processed.jpeg&w=3840&q=75)
Transcribed Image Text:A gas turbine cycle has two stages of
compression, each stage has an isentropic
efficiency of 82%, with an intercooler between
the stages. Air enters the first stage at 100
kPa, 24 C. Air exits the intercooler at 70 C. The
maximum cycle temperature is 1250 C, and
the cycle has a single turbine stage with
pressure ratio of 23 and isentropic efficiency of
90%. The cycle also includes a regenerator
with an effectiveness of 78%. Calculate the
following
Thermal Input heat Compressor
efficiency
Turbine
work
work
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