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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cause moisture and oil vapour to drop out
Reduce volume of air
Remove impurities from air
Cool the air

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

More
Depends on other factors
Same
Less

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the diffuser and impeller
In the impeller only
In the diffuser only
In the inlet guide vanes only

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Axial
Screw
Reciprocating
Centrifugal

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Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁ - v₂)²/g
(v₁² -v₂²)/g
(v₁ - v₂)²/2g
(v₁² -v₂²)/2g

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of thermal efficiency
Increase of work ratio
Both (A) and (B) above
Decrease of work ratio

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