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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?

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

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Before first stage suction
Before the inter-cooler
Between the after-cooler and receiver
After the inter-cooler

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Axial component
Radial component
Tangential component
None of these

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Produces uniform torque
Has more efficiency
All of the listed here
Can be driven at a very high speed

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They are not air breathing engines
They can generate very high thrust
They have high propulsion efficiency
These engines can work on several fuels

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
All of these
Heating chamber
Cooling chamber

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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