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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

None of these
Indicated power
Brake power
Frictional power

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the thermal efficiency
Decreases the thermal efficiency
Increases the compressor work
Increases the turbine work

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Adiabatic compression
Isentropic compression
Isothermal compression
Polytropic compression

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the base
at the tip
in the center
between ~ to i of the blade height

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

All of these
Reheating the air after partial expansion in the turbine
Adding heat exchanger
Injecting water in/around combustion chamber

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Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Backward curved
Forward curved
None of the listed here
Radial

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