Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines - Discussion
Discussion Forum : Compressors, Gas Dynamics and Gas Turbines - Section 1 (Q.No. 26)
26.
In axial flow compressor, exit flow angle deviation from the blade angle is a function of
Discussion:
1 comments Page 1 of 1.
Shiva said:
5 years ago
Please explain it I don't understand.
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