Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines - Discussion

Discussion Forum : Compressors, Gas Dynamics and Gas Turbines - Section 1 (Q.No. 37)
37.
The compression ratio in a gas turbine is
4
1
9
12
Answer: Option
Explanation:
No answer description is available. Let's discuss.
Discussion:
29 comments Page 3 of 3.

ANKIT CHAUDHARI said:   1 year ago
The right answer is 4.

Jitendra Kumar said:   8 years ago
7 is the right answer.

Rama said:   9 years ago
7 is the right answer.

Pradeep gk said:   8 years ago
7 bar is correct.

Sham malik said:   6 years ago
It should be 9.

SANTOSH KUMAR SAHU said:   8 years ago
It Should be 7.

Vinay said:   5 years ago
It is 7 to 9.
(1)

Jnk said:   9 years ago
It is 7 to 9.

Rock said:   9 years ago
It is 9.


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