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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Maximum cycle temperature
Minimum cycle temperature
All of these
Pressure ratio

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow
Increase in flow and decrease in efficiency
Decrease in flow
Increase in efficiency

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Requires no air for its operation
Is self operating at zero flight speed
Is not self operating at zero flight speed
Produces a jet consisting of plasma

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase temperature
Increase speed
Increase power output
Reduce turbine size

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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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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Adiabatic
None of these
Isothermal
Polytropic

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