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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

64 bar
256 bar
1 bar
16 bar

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
High speeds
Low speeds
Low altitudes

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Compressors, Gas Turbines and Jet Engines
In jet engines, paraffin is usually used as the fuel because of its

High calorific value
Low freezing point
Ease of atomisation
Both (A) and (C) above

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In a single cylinder on both sides of the piston
In one cylinder
In two cylinders
In two cylinders on both sides of the piston

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a gas turbine as compared to a diesel plant is

Same
More
Less
Depends on other factors

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Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

p₂/p₁ = p₃/p₂
p₁/p₃ = p₂/p₁
p₁ = p3
p₁ = p₂ p3

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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