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Mechanical Engineering · Q243

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 243

Q243

The compression ratio in a gas turbine is of the order of

A.
3.5 : 1
B.
5 : 1
C.
8 : 1
Answer
D.
12 : 1

Answer: Option C

Solution

Answer: Option C
Solution:
The compression ratio in a gas turbine is of the order of 8 : 1