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Compressors, Gas Turbines and Jet Engines

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

Decrease of heat loss in exhaust
High thermal efficiency
Maximum work output
Reduction in compressor work

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Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Clearance control
Blow off control
Any one of the above
Throttle control

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Radial component
None of these
Tangential component
Axial component

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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
A propeller system
Chemical rocket engine

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Standard air
Compressed air at delivery pressure
Compressed air
Free air

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor without clearance volume, the work-done is maximum during

None of these
Isothermal compression
Polytropic compression
Isentropic compression

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