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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

Indicated power
None of these
Brake power
Frictional power

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Either (A) or (B)
None of these
Electric motor
Engine

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

Surrounding air
None of these
Its own oxygen
Compressed atmospheric air

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

Stainless steel
High alloy steel
Carbon steel
High nickel alloy

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

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

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Decrease
Remain same
Increase
None of these

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