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Compressors, Gas Turbines and Jet Engines

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

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

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

Free air
Compressed air
Standard air
Compressed air at delivery pressure

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Compressors, Gas Turbines and Jet Engines
The inlet pressure is always ___ the discharge pressure.

None of the listed here
More than
Less than
Equal to

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Compressors, Gas Turbines and Jet Engines
The ratio of the volume of free air delivery per stroke to the swept volume of the piston, is known as

Isothermal efficiency
Mechanical efficiency
Compressor efficiency
Volumetric efficiency

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

0.37569444444444
2.5423611111111
0.084027777777778
0.16736111111111

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High speeds
Low speeds
Low altitudes
High altitudes

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