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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Centrifugal type
Axial flow type
Radial flow type
None of these

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

20°C and 1 kg/cm²
Intake temperature and pressure conditions
0°C and 1 kg/cm²
N.T.P. conditions

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Right side of main
Top side of main
Bottom side of main
Left side of main

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To reduce the exit temperature
To increase the output
To save fuel
To increase the efficiency

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Pressure coefficient
Slip factor
Polytropic reaction
Work coefficient

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Compressors, Gas Turbines and Jet Engines
A large clearance volume in a reciprocating compressor results in

Increased volume flow rate
Reduced volume flow rate
Lower delivery pressure
Lower suction pressure

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