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Mechanical Engineering · Q3

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 3

Q3

Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

A.
Higher
B.
Lower
Answer
C.
Equal
D.
Can't be compared

Answer: Option B

Solution

Answer: Option B
Solution:
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is lower
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