Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines - Discussion
Discussion Forum : Compressors, Gas Dynamics and Gas Turbines - Section 2 (Q.No. 21)
21.
The axial flow compressor is preferred in air-craft gas turbines because of
Discussion:
1 comments Page 1 of 1.
Anomie said:
7 years ago
Higher Thrust is the right choice because axial flow compressor produces maximum thrust from back. That causes the flight to move forward.
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