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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

0.084027777777778
0.16736111111111
0.37569444444444
2.5423611111111

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

Index of compressor performance
The ratio of the air actually delivered to the amount of piston displacement
Reciprocal of compression ratio
The ratio of stroke volume to clearance volume

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Compressors, Gas Turbines and Jet Engines
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the

None of these
Both (A) and (B)
Thrust and range of aircraft
Efficiency of the engine

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

Before inter-cooler
After inter-cooler
Between after-cooler and air receiver
After receiver

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Higher average velocities
Aerofoil blades are used
Higher pressure ratio per stage
Larger air handling ability per unit frontal area

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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 minimum during

Isentropic compression
None of these
Isothermal compression
Polytropic compression

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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