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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Equal to zero
Opposite to the direction of motion of blades
Depending on the velocity
In the direction of motion of blades

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At very high speed
At average speed
At very slow speed
At zero speed

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

None of these
Adiabatic
Polytropic
Isothermal

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Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

It requires very big cylinder
It does not increase pressure much
It is impossible in practice
Compressor has to run at very slow speed to achieve it

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Joule cycle
Rankine cycle
Ericsson cycle
Carnot cycle

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