Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber and incidence angle
Space-chord ratio
Blade camber and space-chord ratio
Blade camber

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Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

Decreases net output but increases thermal efficiency
Increases net output and thermal efficiency both
Increases net output but decreases thermal efficiency
Decreases net output and thermal efficiency both

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Compressors, Gas Turbines and Jet Engines
Pick up the correct statement

Gas turbine's blade will appear as impulse section at the hub and as a reaction section at tip
Gas turbines have their blades similar to steam turbine
Gas turbines use both air and liquid cooling
Large gas turbines use radial inflow turbines

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