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Compressors, Gas Turbines and Jet Engines

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

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

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

Minimum cycle temperature
Pressure ratio
All of these
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

Compressor has to run at very slow speed to achieve it
It does not increase pressure much
It is impossible in practice
It requires very big cylinder

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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
Free air
Compressed air

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Reduce turbine size
Increase speed
Increase power output
Increase temperature

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
30 bar
50 bar
20 bar

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