b) What are the following quantities: V2, V3, V4, T2, T3, and T4? c) What is the work done in going from points 1 to 2? d) What is the work done in going from points 3 to 4?
b) What are the following quantities: V2, V3, V4, T2, T3, and T4? c) What is the work done in going from points 1 to 2? d) What is the work done in going from points 3 to 4?
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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Question
Answer B) C) D)

Transcribed Image Text:4)
The process of burning fuel in a turbine engine can be modeled by a heat engine that utilizes a Bray-
ton Cycle. The Brayton Cycle consists of the following steps:
1. Adiabatic compression
2. Isobaric expansion due to heating
3. Adiabatic expansion
4. Isobaric compression
Consider a turbine that starts with an initial pressure P1= 101, 325PA, an initial volume V= 2.0m3,
and an initial temperature of T1= 300.0k. The gas is then compressed adiabatically to a pressure P2=
1, 013, 250PA. Next the gas is allowed to expand isobarically via heating. In the next step the gas
expands adiabatically to a pressure P4= 101, 325PA.
a) Draw a PV diagram for one cycle of this heat engine. Make sure to include the following:
• Label the step with Qh
• Label the step with Qc
• Label the initial point, 2nd point, 3rd point, and the 4th point.
b) What are the following quantities: V2, V3, V4, T2, T3, and T4?
c) What is the work done in going from points 1 to 2?
d) What is the work done in going from points 3 to 4?
rev
e) If the engine operates at 465, what is the power output of this engine?
min
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