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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

May increase or decrease depending on clearance volume
Decrease
Increase
Remain same

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One-half
Same
One fourth
One sixth

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Maximum cycle temperature
Pressure ratio
Minimum cycle temperature
All of these

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Compressors, Gas Turbines and Jet Engines
Mechanical efficiency of gas turbines as compared to I.C engines is

None of these
Lower
Higher
Same

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

More/less depending on compressor capacity
Same
Less
More

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
Gas turbine engine equipped with a propulsive nozzle and diffuse
Chemical rocket engine
A propeller system

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