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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

1 bar and 40°C
0.1 bar and 40°C
0.1 bar and 20°C
1 bar and 20°C

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Inversely proportional to clearance volume
Greatly affected by clearance volume
Not affected by clearance volume
Directly proportional to clearance volume

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Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isothermal compression
Isentropic compression
Polytropic compression
None of the listed here

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Increase
Decrease
Other factors control it
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Larger air handling ability per unit frontal area
Aerofoil blades are used
Higher average velocities
Higher pressure ratio per stage

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

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

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