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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Relief valve
Start-stop motor
Variable speed
Constant speed unloader

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

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

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.045138888888889
0.048611111111111
0.043055555555556
0.00070833333333333

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Compressors, Gas Turbines and Jet Engines
The inlet pressure is always ___ the discharge pressure.

Less than
None of the listed here
Equal to
More than

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

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

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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