Aerospace Engineering > GATE 2010 > Compressor Design
For a multi-stage axial compressor with constant diameter hub
A
Blade height decreases in the flow direction
B
Blade height increases in the flow direction
C
Blade height remains constant
D
Blade height first increases and then decreases in the flow direction

Correct : a

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Related Topics

GATE Aerospace Engineering 2010 GATE Aerospace 2010 Q19 multi stage axial compressor blade height axial compressor constant diameter hub axial compressor flow direction turbomachinery

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