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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
Multi cylinder engine
Gas turbine
4-stroke diesel engine

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

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

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

Low weight and small frontal area
High h.p. and low weight
Small frontal area and high h.p.
High speed and high h.p.

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as adiabatic
Same as isothermal
Better than isothermal and adiabatic
In between isothermal and adiabatic

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Isothermal efficiency
Adiabatic efficiency
Mechanical efficiency
Volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

Indicated power
Brake power
None of these
Frictional power

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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