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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Mass
Energy
Linear momentum
Flow

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

None of these
Its own oxygen
Surrounding air
Compressed atmospheric air

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at

15°C and 1 kg/cm²
20°C and 1 kg/cm² and relative humidity 36%
0°C and standard atmospheric conditions
Atmospheric conditions at any specific location

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as adiabatic
Better than isothermal and adiabatic
Same as isothermal
In between isothermal and adiabatic

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Better mechanical balance
Less power requirement
Less loss of air due to leakage past the cylinder
Lower volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.4
0.2
0.3
0.5

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