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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

1.00 kg/cm²
1.03 kg/cm²
1.06 kg/cm²
0.53 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In a single cylinder on both sides of the piston
In one cylinder
In two cylinders on both sides of the piston
In two cylinders

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Pumps
Axial flow compressors
All of these
Radial flow compressors

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

Temperature rise follows a linear relationship
Temperature during compression remains constant
Work done is maximum
No heat leaves or enters the compressor cylinder during compression

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered in a medium capacity air compressor per unit time is

Above 5 m³/s
None of these
0.15 to 5 m³/s
0.1 to 1.2 m³/s

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

A propeller system
Gas turbine engine equipped with a propulsive nozzle and diffuse
Ramjet engine
Chemical rocket engine

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