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Mechanical Engineering · Q226

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 226

Q226

The axial flow compressor is preferred in aircraft gas turbines because of

A.
Low frontal area
Answer
B.
Higher thrust
C.
High pressure rise
D.
None of these

Answer: Option A

Solution

Answer: Option A
Solution:
The axial flow compressor is preferred in aircraft gas turbines because of Low frontal area