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Compressors, Gas Turbines and Jet Engines

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

Does not require oxygen
Uses compressed atmospheric air
Uses surrounding air
Carries its own oxygen

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Tangential component
Axial component
Radial component
None of these

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

700°C
1000°C
1500°C
2000°C

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

None of the listed here
Critical pressure
Discharge pressure
Back pressure

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

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

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

Stainless steel
High nickel alloy
High alloy steel
Carbon steel

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