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Compressors, Gas Turbines and Jet Engines

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

Increase power output
Increase speed
Increase temperature
Reduce turbine size

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Adiabatically
Isochronically
Isothermally
Isentropically

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Lost work
Reduction of speed of incoming air and conversion of part of it into pressure energy
Increasing speed of incoming air
Compression of inlet air

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Pressure ratio
None of these
Compression ratio
Work ratio

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

20°C and 1 kg/cm²
Intake temperature and pressure conditions
0°C and 1 kg/cm²
N.T.P. conditions

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Carnot cycle
Ericsson cycle
Brayton or Atkinson cycle
Rankine cycle

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