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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

Free air delivery
Compressor capacity
Swept volume
None of these

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

All of the listed here
Can be driven at a very high speed
Has more efficiency
Produces uniform torque

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

The atmosphere
A source of low temperature air
A source of high temperature air
A source at 0° C

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Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Total temperature drop in the stage
Adiabatic temperature drop in the stage
Total temperature drop
Total adiabatic temperature drop

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber
Blade camber and incidence angle
Space-chord ratio
Blade camber and space-chord ratio

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High speed and high h.p.
Small frontal area and high h.p.
High h.p. and low weight
Low weight and small frontal area

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