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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Slip factor
Degree of reaction
Pressure coefficient
Work factor

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Enables compression in two stages
Results in saving of power in compressing a given volume to given pressure
Is the standard practice for big compressors
Cools the delivered air

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

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

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Compressors, Gas Turbines and Jet Engines
Rotary compressor is best suited for

Large quantity of air at high pressure
Large quantity of air at low pressure
Small quantity of air at low pressure
Small quantity of air at high pressure

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

p₁ p₃ = p₂ p₄
p₁ p₂ = p₃ p₄
p₂/p₁ = p₃/p₂ = p₄/p₃
p₃/p₁ = p₄/p₂

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Compressors, Gas Turbines and Jet Engines
In a reciprocating air compressor, the compression work per kg of air

Increases as clearance volume increases
Increases as clearance volume decreases
Decreases as clearance volume increases
Is independent of clearance volume

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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