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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volume of air sucked by the compressor during its suction stroke is called

Compressor capacity
Swept volume
Free air delivery
None of these

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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 sixth
One-half
Same
One fourth

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

Increases the turbine work
Increases the compressor work
Increases the thermal efficiency
Decreases the thermal efficiency

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control output of turbine
Control fire hazards
Increase efficiency
Control temperature

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

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

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Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isothermal compression
Polytropic compression
None of the listed here
Isentropic compression

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