Vidyalelo
Mechanical Engineering · Q27

Compressors, Gas Turbines And Jet Engines

Engineering and GATE · Mechanical Engineering · question 27

Q27

In axial flow compressor, exit flow angle deviation from the blade angle is a function of

A.
Blade camber
B.
Blade camber and incidence angle
Answer
C.
Space-chord ratio
D.
Blade camber and space-chord ratio

Answer: Option B

Solution

Answer: Option B
Solution:
In axial flow compressor, exit flow angle deviation from the blade angle is a function of Blade camber and incidence angle