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
Discussion:
29 comments Page 2 of 3.
Islam gamal said:
7 years ago
I think it means that the compression ratio between the inlet of the whole machine and outlet so what the compressor compresses the turbine expand so the right answer will be 1.
GOPAL DEY said:
7 years ago
The Compression Ratio for Gas turbine is 7.
Vinay agarwal said:
7 years ago
It's 10 to 15 in a gas turbine.
So, 12 is correct guys.
So, 12 is correct guys.
Jitendra Kumar said:
8 years ago
7 is the right answer.
Vicky said:
8 years ago
7 is the correct answer.
ASHISH said:
10 years ago
If the compression ratio is 1 then how does it reduces the pressure of the air before delivering?
SANTOSH KUMAR SAHU said:
8 years ago
It Should be 7.
Nayan Gogoi said:
8 years ago
It should be 7, right? Then why here it is?
Jigar patel said:
8 years ago
Yes, the correct answer is 7.
Ashok said:
8 years ago
If pressure ratio is 1 what is the purpose of using a compressor.
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