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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Plasma
Solids
Liquid
Highly heated atmospheric air

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Can be driven at a very high speed
All of the listed here
Produces uniform torque
Has more efficiency

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

64 bar
256 bar
1 bar
16 bar

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

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

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

700°C
2000°C
1000°C
1500°C

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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