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

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Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Isentropically
Polytropically
Isothermally
None of these

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Back to the compressor
Vacuum
Discharge nozzle

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Both (A) and (B) above
Fully insulating the cylinder
Cold water spray
Multistage compression

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are suitable for

Large discharge at low pressure
Low discharge at low pressure
Low discharge at high pressure
Large discharge at high pressure

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

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

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