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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Same
None of these
Higher
Lower

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

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

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Centrifugal
Axial
Reciprocating
Screw

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

One air stream
No air stream
Two or more air streams
Solid fuel firing

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Lower volumetric efficiency
Less loss of air due to leakage past the cylinder
Better mechanical balance
Less power requirement

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

Adiabatically
Isothermally
Isochronically
Isentropically

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